diff --git a/DesignEvaluator/designEvaluator_conf.xml b/DesignEvaluator/designEvaluator_conf.xml
index f11baa565c5962667153f118e7a00cd31479c6c1..4e5950b5bb43773128a99a5ff22efe0c32ed3e55 100644
--- a/DesignEvaluator/designEvaluator_conf.xml
+++ b/DesignEvaluator/designEvaluator_conf.xml
@@ -5,7 +5,6 @@
<file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020.xml</file_name>
<design_directory Desc="Path" Unit="-" Default="">./test-upstream-files/</design_directory>
</aircraft_design>
- <other_aircraft_designs Desc="Further designs to be compared against the reference (IODir/IOFileName)">1</other_aircraft_designs>
<aircraft_design ID="1">
<name Desc="Name" Unit="-" Default="">CSR nr1</name>
<file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020_0.xml</file_name>
@@ -24,8 +23,9 @@
</program_settings>
<parameters Desc="parameters to be compared">
<something>
- <sub_path ID="1" Name="MTOM">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/mass/value</sub_path>
+ <sub_path ID="0" Name="MTOM">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/mass/value</sub_path>
</something>
+ <sub_path ID="1" Name="Moment of Inertia">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/inertia/j_xx/value</sub_path>
<sub_path ID="2" Name="OME">analysis/masses_cg_inertia/operating_mass_empty/mass_properties/mass/value</sub_path>
<sub_path ID="3" Name="Some Name">requirements_and_specifications/design_specification/propulsion/propulsor@1/energy_carrier_ID/value</sub_path>
<sub_path ID="4" Name="Another Name">requirements_and_specifications/design_specification/propulsion/propulsor@123/energy_carrier_ID/value</sub_path>
diff --git a/DesignEvaluator/src/main.cpp b/DesignEvaluator/src/main.cpp
index 36206415f0616942d17d44efcb584f98c9bf286a..26b779483e2cd8f91450a6d25a24a0b273366b30 100644
--- a/DesignEvaluator/src/main.cpp
+++ b/DesignEvaluator/src/main.cpp
@@ -3,6 +3,17 @@
#include <boost/property_tree/xml_parser.hpp>
#include <boost/property_tree/ptree.hpp>
+// Function to remove a substring from the end of a string
+std::string substractStringFromEnd(const std::string& string, const std::string& string_to_substract) {
+ if (string.size() >= string_to_substract.size() &&
+ string.compare(string.size() - string_to_substract.size(), string_to_substract.size(), string_to_substract) == 0) {
+ // If the string ends with the substring, remove it
+ return string.substr(0, string.size() - string_to_substract.size());
+ }
+ // Otherwise, return the original string unchanged
+ return string;
+}
+
void printPtree(const boost::property_tree::ptree &tree, const std::string &prefix = "") {
for (const auto &node : tree) {
// Print current node name
@@ -238,6 +249,7 @@ int main () {
std::string node_path{"aircraft_exchange_file/" + node.second.data()};
double upstream_value{NAN};
double local_value{NAN};
+ std::string unit{"?"};
if (containsSymbol(node_path, "@")) {
std::string pre{node_path.substr(0, node_path.find_first_of('@'))};
@@ -248,18 +260,22 @@ int main () {
boost::property_tree::ptree temp_upstream_tree{GetSubtreeByAttributevalue(aircraft_design_trees.at(0), pre, "ID", attribute_value)};
boost::property_tree::ptree temp_local_tree{GetSubtreeByAttributevalue(tree, pre, "ID", attribute_value)};
+ boost::property_tree::ptree temp_unit_tree{GetSubtreeByAttributevalue(tree, pre, "ID", attribute_value)};
upstream_value = temp_upstream_tree.get<double>(boost::property_tree::ptree::path_type(post, '/'));
local_value = temp_local_tree.get<double>(boost::property_tree::ptree::path_type(post, '/'));
+ unit = temp_unit_tree.get<std::string>(boost::property_tree::ptree::path_type(substractStringFromEnd(post, "value") + "unit", '/'));
} else {
upstream_value = aircraft_design_trees.at(0).get<double>(boost::property_tree::ptree::path_type(node_path, '/'));
local_value = tree.get<double>(boost::property_tree::ptree::path_type(node_path, '/'));
+ unit = tree.get<std::string>(boost::property_tree::ptree::path_type(substractStringFromEnd(node_path, "value") + "unit", '/'));
}
temp_tree.put(node.second.get<std::string>("<xmlattr>.Name"), upstream_value - local_value);
+ temp_tree.put(node.second.get<std::string>("<xmlattr>.Name") + ".<xmlattr>.unit", unit);
}
result_tree.push_back(temp_tree);
- }
+ }
}
catch(const std::exception& e)
{
@@ -278,24 +294,57 @@ int main () {
std::cout << "Current State: " << state << std::endl;
// Write Output
+ // Create header
+ boost::property_tree::ptree output_tree{};
+ output_tree.put("html.<xmlattr>.lang", "en");
+ output_tree.put("html.head.meta.<xmlattr>.content", "width=device-width, initial-scale=1.0");
+ output_tree.put("html.head.meta.<xmlattr>.name", "viewport");
+ output_tree.put("html.head.meta.<xmlattr>.charset", "utf-8");
+ output_tree.put("html.head.title", "<probably same as report name>");
+ output_tree.put("html.head.link.<xmlattr>.href", "style.css");
+ output_tree.put("html.head.link.<xmlattr>.rel", "stylesheet");
+
+ // Create body
+ boost::property_tree::ptree temp_tree{};
+ temp_tree.put("<xmlattr>.class", "content");
+ temp_tree.put("h1", "Report - <some name>");
+ temp_tree.put("div.<xmlattr>.class", "container");
+ // Create data tables
+ unsigned int aircraft_counter{0};
for (const auto& tree : result_tree) {
- printPtree(tree);
+ ++aircraft_counter;
+ boost::property_tree::ptree data_tree{};
+ data_tree.put("<xmlattr>.class", "box data");
+ boost::property_tree::ptree my_tree{GetSubtreeByAttributevalue(program_settings_tree, "aircraft_design", "ID", std::to_string(aircraft_counter))};
+ std::string myString{my_tree.get<std::string>("name")};
+ data_tree.put("h2", myString);
+ data_tree.put("table.<xmlattr>.class", "content-table");
+ data_tree.put("table.caption", "Residual Values");
+ data_tree.put("table.thead", "");
+ data_tree.put("table.tbody", "");
+ boost::property_tree::ptree thead{};
+ thead.add_child("th", boost::property_tree::ptree{"paramter"});
+ // thead.add_child("th", boost::property_tree::ptree{"symbol"});
+ thead.add_child("th", boost::property_tree::ptree{"value"});
+ thead.add_child("th", boost::property_tree::ptree{"unit"});
+ data_tree.add_child("table.thead.tr", thead);
+ for (const auto& node : tree) {
+ boost::property_tree::ptree tbody{};
+ tbody.add_child("td", boost::property_tree::ptree{node.first});
+ tbody.add_child("td", boost::property_tree::ptree{node.second.data()});
+ tbody.add_child("td", boost::property_tree::ptree{node.second.get<std::string>("<xmlattr>.unit")});
+ data_tree.add_child("table.tbody.tr", tbody);
+ }
+ temp_tree.add_child("div.div", data_tree);
}
-
-
-
- // Questions:
- // - Name of the dispalyed value? ANS: from config file
- // Curretnly form config file, but if from acft_ex_file name will always be "value"
- //
- // - Output format? ANS: .html format
- // - Where to get the file directories from? ANS: from config file program settings
-
- // Next steps:
- // - read file locations from config.xml
- // - output as .html
- // - multiple file comparisons
-
+ output_tree.add_child("html.body.div", temp_tree);
+
+ // Write .html file
+ boost::property_tree::xml_writer_settings<std::string> settings(' ', 4); // 4 spaces for indentation
+ boost::property_tree::write_xml("./projects/reporting/reportHTML/ReportXYZ.html",
+ output_tree,
+ std::locale(),
+ settings);
state = State::ProgrammFinished;
break;
@@ -308,8 +357,21 @@ int main () {
}
default: {
+ // TODO(Oli): check why when nodes have the same name only one is printed in the result_tree
+
+ // Questions:
+ // where are filepath of output.html and config.xml specified?
+
break;
}
}
}
-}
\ No newline at end of file
+}
+
+/*
+ for (auto element : result_tree) {
+ std::cout << "TREE: " << std::endl;
+ printPtree(element);
+ std::cout << std::endl;
+ }
+*/
\ No newline at end of file
diff --git a/projects/newFormat-CSMR-2020_0.xml b/projects/newFormat-CSMR-2020_0.xml
index 925455677c2ec5c63db49b40a49280c4566277ae..66080faee70b70238a5acf80a9a3b7726dd5daa0 100644
--- a/projects/newFormat-CSMR-2020_0.xml
+++ b/projects/newFormat-CSMR-2020_0.xml
@@ -794,7 +794,7 @@
<mass_properties description="maximum takeoff mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
- <value>1510141.8121567257</value>
+ <value>1500000</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -869,7 +869,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>0</value>
+ <value>77777</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -955,7 +955,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>0</value>
+ <value>3456</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
diff --git a/projects/newFormat-CSMR-2020_1.xml b/projects/newFormat-CSMR-2020_1.xml
index 57d3fe34c5d441d2427ba084ee1f6896428ff72d..bc38bb004f0b6bd040cb9dfd9832d09f20670a99 100644
--- a/projects/newFormat-CSMR-2020_1.xml
+++ b/projects/newFormat-CSMR-2020_1.xml
@@ -794,7 +794,7 @@
<mass_properties description="maximum takeoff mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
- <value>1510141.8121567257</value>
+ <value>1400000</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -869,7 +869,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>0</value>
+ <value>345345</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -955,7 +955,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>0</value>
+ <value>756756</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
diff --git a/projects/newFormat-CSMR-2020_2.xml b/projects/newFormat-CSMR-2020_2.xml
index 69740601c7ed2965d1d4747f03478c30bf64f6ee..6e7c01354f0b01b7aaedfd7727c14785cbead624 100644
--- a/projects/newFormat-CSMR-2020_2.xml
+++ b/projects/newFormat-CSMR-2020_2.xml
@@ -794,7 +794,7 @@
<mass_properties description="maximum takeoff mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
- <value>1510141.8121567257</value>
+ <value>1510141.0</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -869,7 +869,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>0</value>
+ <value>3209</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
diff --git a/projects/oldFormat-CSR.xml b/projects/oldFormat-CSR.xml
deleted file mode 100644
index 6b4c8683fbe9007cce157f079ec5ee5b10ec17e7..0000000000000000000000000000000000000000
--- a/projects/oldFormat-CSR.xml
+++ /dev/null
@@ -1,3866 +0,0 @@
-<AcftExchangeFile>
- <General Desc="Allgemeine Angaben">
- <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
- <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-01</Model>
- </General>
- <MassesAndLoadings Desc="-">
- <MassBreakdown Desc="Massenverteilung">
- <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
- <Mass ToolLevel="1" Unit="kg">8535.455741</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4">
- <Mass ToolLevel="1" Unit="kg">6278.799947</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor>
- <EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor>
- <EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor>
- </CenterWing>
- <WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8">
- <Mass ToolLevel="1" Unit="kg">2256.655794</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
- <Mass ToolLevel="1" Unit="kg">291.6450898</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FixedLeadingEdge>
- <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
- <Mass ToolLevel="1" Unit="kg">373.9546469</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </MovableLeadingEdge>
- <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
- <Mass ToolLevel="1" Unit="kg">582.2672595</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FixedTrailingEdge>
- <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
- <Mass ToolLevel="1" Unit="kg">1008.788798</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </MovableTrailingEdge>
- </WingLEandTE>
- <Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9">
- <Mass ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </Miscellaneous>
- </Wing>
- <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
- <Mass Desc="-" ToolLevel="1" Unit="kg">8888.102165</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Fuselage>
- <Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements">
- <Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1257.118042</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.40806564</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- <Tailplane Desc="Airbus Chapter 13">
- <Mass ToolLevel="1" Unit="kg">705.5278242</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.73963722</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- </Tailplane>
- <Fin Desc="Airbus Chapter 14">
- <Mass Desc="-" ToolLevel="1" Unit="kg">551.5902181</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">32.98395918</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- </Fin>
- </Empennage>
- <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2518.773274</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.32982807</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.469648031</h_Item>
- </RefPoint>
- <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">377.8159911</TotalMass>
- <RefPoint Desc="Position of NoseGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
- <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
- <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
- <RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
- <RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- </LandingGear>
- <Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1049.543431</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.59758377</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.838904205</h_Item>
- </RefPoint>
- </Pylons>
- <PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit">
- <Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">7983.304178</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.56488425</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.882731847</h_Item>
- </RefPoint>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
- <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2237.636365</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2">
- <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <BleedAirSystem Desc="Airbus Chapter 21, ATA36">
- <Mass Desc="-" ToolLevel="1" Unit="kg">170.4663501</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </BleedAirSystem>
- <EngineControls Desc="Airbus Chapter 22">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineControls>
- <FuelSystem Desc="Airbus Chapter 25, ATA28">
- <Mass Desc="-" ToolLevel="1" Unit="kg">313.2402355</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FuelSystem>
- </PowerUnit>
- <Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
- <Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5309.46001</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.22640698</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-0.5973844066</h_Item>
- </RefPoint>
- <APU Desc="Airbus Chapter 30, ATA49">
- <Mass Desc="-" ToolLevel="1" Unit="kg">269.6524446</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">35.12321805</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </APU>
- <HydraulicGeneration Desc="Airbus Chapter 31, ATA 29">
- <Mass Desc="-" ToolLevel="1" Unit="kg">177.4943728</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </HydraulicGeneration>
- <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
- <Mass Desc="-" ToolLevel="1" Unit="kg">795.934215</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </HydraulicDistribution>
- <AirConditioning Desc="Airbus Chapter 33, ATA21">
- <Mass Desc="-" ToolLevel="1" Unit="kg">711.2165166</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </AirConditioning>
- <DeIcing Desc="Airbus Chapter 34, ATA30">
- <Mass Desc="-" ToolLevel="1" Unit="kg">41.98276817</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </DeIcing>
- <FireProtection Desc="Airbus Chapter 35, ATA26">
- <Mass Desc="-" ToolLevel="1" Unit="kg">92.36094204</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </FireProtection>
- <FlightControls Desc="Airbus Chapter 36, ATA27">
- <Mass Desc="-" ToolLevel="1" Unit="kg">699.137886</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- <Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
- <Mass Desc="-" ToolLevel="1" Unit="kg">42.43977661</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Roll>
- <Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1">
- <Mass Desc="-" ToolLevel="1" Unit="kg">97.75474213</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Yaw>
- <Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2">
- <Mass Desc="-" ToolLevel="1" Unit="kg">30.4466164</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Pitch>
- <MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3">
- <Mass Desc="-" ToolLevel="1" Unit="kg">63.38988998</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </MovableHorizontalTail>
- <Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4">
- <Mass Desc="-" ToolLevel="1" Unit="kg">143.8595475</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Flaps>
- <SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.5">
- <Mass Desc="-" ToolLevel="1" Unit="kg">38.76193929</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SpoilersAirbrakesLiftdumpers>
- <Slats Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.6">
- <Mass Desc="-" ToolLevel="1" Unit="kg">142.6577969</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Slats>
- <CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7">
- <Mass Desc="-" ToolLevel="1" Unit="kg">139.8275772</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </CommonInstallation>
- </FlightControls>
- <Instruments Desc="Airbus Chapter 37, ATA31">
- <Mass ToolLevel="1" Unit="kg">85.16128872</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.34075992</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Instruments>
- <AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22">
- <Mass ToolLevel="1" Unit="kg">138.3870942</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </AutomaticFlightSystem>
- <Navigation Desc="Airbus Chapter 39, ATA34">
- <Mass Desc="-" ToolLevel="1" Unit="kg">564.1935378</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Navigation>
- <Communication Desc="Airbus Chapter 40, ATA23">
- <Mass Desc="-" ToolLevel="1" Unit="kg">276.7741884</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Communication>
- <ElectricalGeneration Desc="Airbus Chapter 41, ATA24">
- <Mass Desc="-" ToolLevel="1" Unit="kg">774.2507101</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </ElectricalGeneration>
- <ElectricalDistribution Desc="Airbus Chapter 42, ATA24">
- <Mass Desc="-" ToolLevel="1" Unit="kg">682.914046</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </ElectricalDistribution>
- </Systems>
- <Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings">
- <Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3114.623325</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Furnishing Desc="Airbus Chapter 50, ATA25">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2464.223172</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Furnishing>
- <FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35">
- <Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </FixedEmergencyOxygen>
- <Lighting Desc="Airbus Chapter 52, ATA33">
- <Mass Desc="-" ToolLevel="1" Unit="kg">261.9261532</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Lighting>
- <WaterInstallation Desc="Airbus Chapter 53, ATA38">
- <Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WaterInstallation>
- </Furnishings>
- <OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items">
- <Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3326.415065</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.54754916</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1575.865065</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.5703719</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OperatorEquipment>
- <OperationalEquipment Desc="Airbus Chapter 61 (movable equipment)">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.72658107</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OperationalEquipment>
- </OperatorsItems>
- <NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </NotAllocated>
- </MassBreakdown>
- <MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM>
- <MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">65025.01668</MLM>
- <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">80000</MTOM>
- <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
- <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38656.38017</MME>
- <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">999</OME>
- <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">61982.79523</MZFM>
- <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
- <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">31084.34394</MaximumUsableFuel>
- <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">628.681385</WingLoading>
- <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3218120393</ThrustToWeight>
- <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
- <MomentsOfInertia Desc="Flaechentraegheitsmomente">
- <Ixx Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixx>
- <Iyy Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyy>
- <Izz Desc="-" ToolLevel="1" Unit="kg*m2">0</Izz>
- <Ixy Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixy>
- <Ixz Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixz>
- <Iyz Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyz>
- </MomentsOfInertia>
- <CentreOfGravityRange Desc="Schwerpunktsgrenzen">
- <TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7359472859</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.56950713</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </TrimRefPt>
- <ForwardLimit Desc="Vorderste Schwerpunktlage">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9505895064</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.4584795</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </ForwardLimit>
- <AftLimit Desc="Hinterste Schwerpunktlage">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-1.011726725</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.65854294</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </AftLimit>
- </CentreOfGravityRange>
- </MassesAndLoadings>
- <Geometry Desc="Geometriebeschreibung">
- <UsedElements Desc="Liste der verwendeten Geometrieelemente">
- <LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces>
- <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface>
- <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface>
- <VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces>
- <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface>
- <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface>
- <Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages>
- <Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage>
- <Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle>
- <Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon>
- <Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear>
- </UsedElements>
- <LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing">
- <SurfaceRefPoint Desc="position of wing to global point of reference">
- <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Surface>
- <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of lifting surface geometry">
- <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
- <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
- <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface>
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints>
- <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_15.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">6.969546741</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.363049953</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.115537999</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_11.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.363049953</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.036840684</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">11.93625533</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2062430536</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- </SurfaceParameters>
- </LiftingSurface>
- <LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser">
- <SurfaceRefPoint Desc="position of wing to global point of reference">
- <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.1606612</r_Surface>
- <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of lifting surface geometry">
- <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
- <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
- <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.140234056</i_Surface>
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.962556849</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.11563951</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.392179667</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- </SurfaceParameters>
- </LiftingSurface>
- <VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin">
- <SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.20843962</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.692105859</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of vertical surface geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.914778427</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.564960467</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">7.105751949</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- </ControlDeviceSetup>
- </SurfaceParameters>
- </VerticalSurface>
- <Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage">
- <FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference">
- <r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage>
- <y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage>
- <h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage>
- </FuselageRefPoint>
- <FuselageParameters Desc="parametric description of the fuselage">
- <NoseDescription>
- <NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments>
- <TipSegment>
- <h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5351396212</h_Tip>
- </TipSegment>
- <NoseSegment ID="1">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6205763694</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.6626671728</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06782437376</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5351396212</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="2">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.229534829</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.312928447</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.2034731213</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4376004301</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="3">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.814885649</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.937980885</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3391218688</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3438425644</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="4">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.363843474</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.524171961</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4747706164</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2559139029</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="5">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.862283086</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.05641841</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.6104193639</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1760769356</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="6">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.293963779</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.517377993</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7460681114</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1069329983</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="7">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.639314251</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.886151978</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.8817168589</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05161690045</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="8">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.873337327</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136047749</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.017365606</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01413253478</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="9">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.153014354</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment>
- </NoseSegment>
- </NoseDescription>
- <MidSectionDescription>
- <MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments>
- <MidSectionSegment ID="1">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">15.57908662</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
- </MidSectionSegment>
- <MidSectionSegment ID="2">
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
- </MidSectionSegment>
- </MidSectionDescription>
- <TailDescription>
- <TailSegments Desc="No of tail segments" ToolLevel="1">7</TailSegments>
- <TailSegment ID="1">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.163206861</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.0335288931</deltah_Segment>
- </TailSegment>
- <TailSegment ID="2">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
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- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle">
- <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
- <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
- <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
- </NacelleRefPoint>
- <NacelleParameters Desc="parametric description of the nacelle">
- <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
- <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
- <InletSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
- <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <NacelleSegment ID="2">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <ExitSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle">
- <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
- <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
- <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
- </NacelleRefPoint>
- <NacelleParameters Desc="parametric description of the nacelle">
- <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
- <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
- <InletSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
- <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <NacelleSegment ID="2">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <ExitSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.219203967</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.219203967</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.023847396</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.834540304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
- </Wheel>
- </Gear>
- </Geometry>
- <Structure Desc="Strukturdaten"></Structure>
- <Accommodation Desc="Kabineneinrichtung">
- <PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal>
- <FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew>
- <CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew>
- <Seats Desc="Description of seats">
- <NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">5</NoOfSeatTypes>
- <seat Desc="Description of seat" ID="1">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">commuter</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">1</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="5">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="2">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="3">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">GeneralAviation</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25.1</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="4">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="5">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">first</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">21.25</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">42.5</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- </Seats>
- <Galleys Desc="Description of galleys">
- <NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes>
- <Gal Desc="Description of galley" ID="1">
- <nameGalley Desc="Name of galley" ToolLevel="1">large_galley</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power>
- </Gal>
- <Gal Desc="Description of galley" ID="2">
- <nameGalley Desc="Name of galley" ToolLevel="1">small_galley</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power>
- </Gal>
- <Gal Desc="Description of galley" ID="3">
- <nameGalley Desc="Name of galley" ToolLevel="1">0</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">0</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">0</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">0</power>
- </Gal>
- </Galleys>
- <Lavatories Desc="Description of lavatories">
- <NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes>
- <Lav Desc="Description of lavatory" ID="1">
- <nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory>
- <NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories>
- <mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass>
- </Lav>
- </Lavatories>
- <Cabin Desc="Beschreibung der Kabine">
- <V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">190.47918</V_AirConditioned>
- <CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks>
- <CabinDeck Desc="Parameter eines Kabinendecks" ID="1">
- <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">95.53300238</A_CabinDeck>
- <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
- <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.613074406</w_CabinDeck>
- <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.44091752</l_CabinDeck>
- <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">185.9285625</V_CabinDeck>
- <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck>
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">6.044387137</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.2648459</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- </CabinDeck>
- <CabinDeck Desc="Parameter eines Kabinendecks" ID="2">
- <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">0</A_CabinDeck>
- <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">0</h_CabinDeck>
- <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">0</w_CabinDeck>
- <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">0</l_CabinDeck>
- <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">0</V_CabinDeck>
- <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">0</PAX_CabinDeck>
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">0</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- </CabinDeck>
- </Cabin>
- <Cargo Desc="Beschreibung des Frachtraums">
- <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">33.22757663</V_Cargo>
- <CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks>
- <CargoDeck Desc="Parameter eines Frachtdecks" ID="1">
- <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">55.02284727</A_CargoDeck>
- <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
- <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.252922327</w_CargoDeck>
- <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">16.91489736</l_CargoDeck>
- <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">34.30498624</V_CargoDeck>
- <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.17849076</V_BulkCargo>
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.69</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.22</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">23.42652858</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- </CargoDeck>
- <CargoDeck Desc="Parameter eines Frachtdecks" ID="2">
- <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">0</A_CargoDeck>
- <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">0</h_CargoDeck>
- <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">0</w_CargoDeck>
- <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">0</l_CargoDeck>
- <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">0</V_CargoDeck>
- <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">0</V_BulkCargo>
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">0</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- </CargoDeck>
- </Cargo>
- </Accommodation>
- <Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)">
- <NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes>
- <Engine Desc="Triebwerks-/Motortyp" ID="1">
- <TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine>
- <EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel>
- <NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines>
- <ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.039876757</ScaleEngines>
- <ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow>
- <EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">V2527-A5/V2527-A5.xml</EngineDataFile>
- <JetEngineData Desc="Jet spezifische Triebwerksdaten">
- <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">121.4507148</SeaLevelStaticThrust>
- <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.613</FanDiameter>
- </JetEngineData>
- <TurbopropEngineData Desc="Prop spezifische Triebwerksdaten">
- <Prop Desc="Propellerdaten">
- <PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter>
- <PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch>
- <Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness>
- </Prop>
- <P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp>
- </TurbopropEngineData>
- <EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk">
- <w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.829</w_Engine>
- <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.118</h_Engine>
- <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.508</l_Engine>
- </EngineDimensions>
- <NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0">
- <InnerNacelle>
- <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
- <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
- <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
- <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
- <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
- <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
- </InnerNacelle>
- <OuterNacelle>
- <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
- <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
- <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
- <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
- <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
- <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
- </OuterNacelle>
- </NacelleRescaling>
- <ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks">
- <EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+15, SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">121.6192213</EquivalentThrust>
- <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">121.4507148</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.255306839</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01033593619</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.027199488</N1>
- </MaximumTakeOff>
- <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">97.29537705</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.274976051</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01310417914</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.02423458</N1>
- </MaximumGoAround>
- <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+0 bei" Mach="0.78">
- <MaxThrust Desc="Without Offtakes">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">35.65209987</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.6237266005</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01749480683</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1</N1>
- </MaxThrust>
- <BucketThrust Desc="Without Offtakes">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.92001194</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4343473894</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01675722181</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.875</N1>
- </BucketThrust>
- <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.97268447</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4521939534</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01741036641</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.905</N1>
- </BucketThrustOfftakes>
- </MaximumContinous>
- </ScaledPerformanceCharacteristics>
- <UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird">
- <UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines>
- <NacelleID ID="1" ToolLevel="1">0</NacelleID>
- <NacelleID ID="2" ToolLevel="1">0</NacelleID>
- <NacelleID ID="3" ToolLevel="1">0</NacelleID>
- <NacelleID ID="4" ToolLevel="1">0</NacelleID>
- </UsedForNacelles>
- </Engine>
- </Propulsion>
- <Systems>
- <FuelTank Desc="Tank system Parameters">
- <CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks>
- <CentreTank Desc="Center-Tank Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83307738</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330577781</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">10165.96362</TankVolume>
- </CentreTank>
- <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
- <WingTank Desc="Fluegeltank-Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">6.308425637</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
- </WingTank>
- <WingTank Desc="Fluegeltank-Beschreibung" ID="2">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">-6.308425637</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
- </WingTank>
- <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
- <TrimTank Desc="Trimmtank-Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">0</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">0</TankVolume>
- </TrimTank>
- <TotalFuelVolume Desc="Gesamtes Kraftstoffvolumen aller Tanks" ToolLevel="1" Unit="l">39597.89037</TotalFuelVolume>
- </FuelTank>
- <ATA21_EnvironmentalControlSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.96155032</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.315916839</BleedAir>
- </DesignPower>
- <AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax>
- <Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation>
- </ATA21_EnvironmentalControlSystem>
- <ATA22_AutoFlight>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA22_AutoFlight>
- <ATA23_Communication>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA23_Communication>
- <ATA24_ElectricSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA24_ElectricSystem>
- <ATA25_Furnishing>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA25_Furnishing>
- <ATA26_FireProtection>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA26_FireProtection>
- <ATA27_FlightControlSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">95.17958985</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA27_FlightControlSystem>
- <ATA28_FuelSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">11.89508876</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA28_FuelSystem>
- <ATA29_HydraulicSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.171489811</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- <Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure>
- </ATA29_HydraulicSystem>
- <ATA30_IceRainProtection>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.128183366</BleedAir>
- </DesignPower>
- </ATA30_IceRainProtection>
- <ATA31_Instrumentation>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA31_Instrumentation>
- <ATA32_LandingGear>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">67.03267969</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA32_LandingGear>
- <ATA33_Lights>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.96874401</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA33_Lights>
- <ATA34_Navigation>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA34_Navigation>
- <ATA35_Oxygen>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA35_Oxygen>
- <ATA36_BleedAir>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1286368529</BleedAir>
- </DesignPower>
- </ATA36_BleedAir>
- <ATA49_APU>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir>
- </DesignPower>
- </ATA49_APU>
- <ATA70_PropulsionSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-142.0813445</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-174.2129642</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.708144271</BleedAir>
- </DesignPower>
- </ATA70_PropulsionSystem>
- </Systems>
- <Aerodynamics Desc="Aerodynamik">
- <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">17.07161371</LoverD_Cruise>
- <LiftCoefficients Desc="Auftriebsbeiwerte">
- <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5388392246</C_L_design>
- <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.910828613</C_LmaxLanding>
- <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.511580029</C_LmaxT-O>
- <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.534</C_LoptimumCruise>
- <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.56482909</C_L_opt_wing>
- <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03082906473</C_L_opt_stab>
- <C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll>
- </LiftCoefficients>
- <DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)">
- <C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03127999549</C_D_total>
- <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.01011147857</C_D_ind>
- <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
- <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01998021606</C_D_visc_total>
- <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.006065898162</C_D_visc_wing>
- <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001539217794</C_D_visc_stab>
- <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001759127689</C_D_visc_fin>
- <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006881721154</C_D_visc_fus>
- <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001626766969</C_D_visc_nac>
- <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.002107484288</C_D_visc_misc>
- </C_D_visc>
- <C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-">
- <C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_total>
- <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_wing>
- <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0</C_D_wave_stab>
- </C_D_wave>
- <EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor>
- </DragCoefficients>
- <MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)">
- <C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">-0.001284519415</C_M_total>
- </MomentCoefficients>
- <Polar Desc="Flugzeugpolare">
- <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">CSR_polar.xml</PolarFile>
- <Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration>
- </Polar>
- <ReferenceValues Desc="Aerodynamische Bezugsgroessen">
- <b Desc="Total wing span" ToolLevel="1" Unit="m">34.10358666</b>
- <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.331683874</MAC>
- <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">122.4268024</S_ref>
- </ReferenceValues>
- <MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor>
- </Aerodynamics>
- <StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit">
- <Stabiliser>
- <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.03545133</VolumeCoefficient>
- <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.46074351</S_ref>
- </Stabiliser>
- <VerticalTail>
- <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.1018345125</VolumeCoefficient>
- <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">26.57458461</S_ref>
- </VerticalTail>
- </StabilityAndControlCharacteristics>
- <Performance Desc="Flugleistungen">
- <Range Desc="Reichweiten">
- <Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3043.938845</Range_maxPayloadatMTOM>
- <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">11558.21333</Range_maxFuelatMTOM>
- <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">3895.43595</Payload_maxFuelatMTOM>
- <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">12572.68487</Range_maxFuelEmpty>
- </Range>
- <Speed Desc="Fluggeschwindigkeiten">
- <M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise>
- <M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating>
- <V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating>
- <M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive>
- <V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive>
- <V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">161.952013</V_s1g>
- </Speed>
- <Altitudes Desc="Flughoehen">
- <h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise>
- <h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified>
- <h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">12010.7005</h_maxOperating>
- <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">12053.19642</h_maxCeiling>
- <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">7730.61576</h_maxOEI>
- </Altitudes>
- <Climb Desc="Steigflug">
- <TTC_Design Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">14.56137643</TTC_Design>
- <Time_to_1500ft_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10>
- <Time_to_ICA_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">15.53402313</Time_to_ICA_ISA10>
- <Range_to_ICA_ISA10 Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="NM">89.09881839</Range_to_ICA_ISA10>
- <Fuel_to_ICA_ISA10 Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="kg">1577.91233</Fuel_to_ICA_ISA10>
- <TTC_ISA Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA>
- <Time_to_1500ft_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA>
- <Time_to_ICA_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA>
- <Range_to_ICA_ISA Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA>
- <Fuel_to_ICA_ISA Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA>
- <TTC_ISA10_optROC Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA10_optROC>
- <Time_to_1500ft_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10_optROC>
- <Time_to_ICA_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA10_optROC>
- <Range_to_ICA_ISA10_optROC Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA10_optROC>
- <Fuel_to_ICA_ISA10_optROC Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA10_optROC>
- </Climb>
- <TakeOff Desc="Start Performance">
- <TakeOffDistance_Normal Desc="Startstrecke - Normalstartstrecke bei MTOM und ISA+15" ToolLevel="2" Unit="m">1731.705965</TakeOffDistance_Normal>
- <BFL Desc="Startstrecke - Balanced Fieldlength bei MTOM und ISA+15 " ToolLevel="2" Unit="m">1853.411621</BFL>
- <TimeToScreenHeight Desc="Zeit bis zum erreichen von 35 ft" ToolLevel="2" Unit="s">34.72221827</TimeToScreenHeight>
- <V_LOF Desc="Abhebegeschwindigkeit" ToolLevel="2" Unit="KCAS">136.8991062</V_LOF>
- <V_1 Desc="Decision Speed bei fuer MTOM BLFL" ToolLevel="2" Unit="KCAS">135.3462489</V_1>
- <V_2 Desc="Geschwindigkeit auf Screen height (35 ft)" ToolLevel="2" Unit="KCAS">136.8991062</V_2>
- <V_FTO Desc="Geschwindigkeit am Ende des Final T-O Segment (1500 ft)" ToolLevel="2" Unit="KCAS">203.0413711</V_FTO>
- <ScdSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.68313876</ScdSegmentClimbGradient>
- <FinalSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.683126144</FinalSegmentClimbGradient>
- </TakeOff>
- <Landing>
- <LandingDistance Desc="Landestrecke" ToolLevel="2" Unit="m">1528.071526</LandingDistance>
- <V_Approach Desc="Anfluggeschwindigkeit" ToolLevel="2" Unit="KCAS">129.2323788</V_Approach>
- </Landing>
- <MissionAnalysis Desc="Missionsanalyse">
- <DesignMission Desc="Parameter der Design-Mission">
- <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionDesign.xml</MissionFile>
- <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5008065466</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">18070.1076</Missionfuel>
- <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">14883.27019</Tripfuel>
- <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
- <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
- <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.947085161</Blocktime>
- <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.713751827</Flighttime>
- <Range Desc="Range" ToolLevel="3" Unit="NM">2500.55303</Range>
- <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">76962.57512</TOM>
- <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload>
- <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
- <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass>
- <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
- <Offtakes>
- <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
- <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">73.40008433</ShaftPowerTotal>
- <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
- </AverageCruiseOfftakes>
- </Offtakes>
- <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
- <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5148367758</CL_avg>
- <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4915188994</CL_min>
- <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5675400636</CL_max>
- </LiftCoefficientsCruise>
- <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
- <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">75060.13292</Mass_TOC>
- <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">62441.91279</Mass_TOD>
- </MassesCruise>
- </DesignMission>
- <StudyMission Desc="Parameter der Study-Mission">
- <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionStudy.xml</MissionFile>
- <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">5967.411758</Missionfuel>
- <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3241.768614</Tripfuel>
- <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
- <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
- <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.50538405</Blocktime>
- <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.272050716</Flighttime>
- <Range Desc="Range" ToolLevel="3" Unit="NM">500.546566</Range>
- <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">61467.87928</TOM>
- <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload>
- <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
- <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass>
- <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
- <Offtakes>
- <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
- <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">72.97412478</ShaftPowerTotal>
- <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
- </AverageCruiseOfftakes>
- </Offtakes>
- <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
- <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4681348875</CL_avg>
- <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4621586298</CL_min>
- <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4991350396</CL_max>
- </LiftCoefficientsCruise>
- <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
- <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">60071.12337</Mass_TOC>
- <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">58584.28057</Mass_TOD>
- </MassesCruise>
- </StudyMission>
- </MissionAnalysis>
- <RequirementsChecks>
- <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionReq.xml</MissionFile>
- <TLARs>
- <TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design>
- <LDN_Design Checked="1" ToolLevel="2">1</LDN_Design>
- <V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design>
- <h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design>
- <h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating>
- <h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI>
- <M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design>
- <TTC_Design Checked="1" ToolLevel="3">1</TTC_Design>
- </TLARs>
- <Certification>
- <climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment>
- <climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment>
- <climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI>
- <climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO>
- </Certification>
- </RequirementsChecks>
- </Performance>
- <MonetaryValues Desc="Kosten und Preise">
- <MonetaryScenario>
- <AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">12079799</AirframeEngineeringHours>
- <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">1500</ProductionVolume>
- </MonetaryScenario>
- <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">28158406</Earnings>
- <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">33855.557</NPV>
- <Prices Desc="Preise">
- <PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">71228241.8</PriceAirplane>
- <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0.07</DiscountRate>
- </Prices>
- <LCC Desc="Life Cycle Costs">
- <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
- <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">3475793421</NRCTotal>
- <NRCComponents>
- <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">1359777460</AirframeEngAndDesign>
- <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">345988343</DevSupportAndTesting>
- <FlightTestAC>
- <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">1636269510</FlightTestACTotal>
- <FlightTestACComponents>
- <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">117031730</EngineAndAvionics>
- <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">622590665</LaborManufacturing>
- <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">188900611</MaterialManufacturing>
- <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">624941946</Tooling>
- <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">82804558</QualityControl>
- </FlightTestACComponents>
- </FlightTestAC>
- <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">133758109</FlightTestOp>
- <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
- </NRCComponents>
- </NonRecurringCosts>
- <RecurringCosts Desc="Recurring Costs">
- <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">35766663</RCTotal>
- <RCComponents>
- <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">2408072</Wing>
- <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">2957731</Fuselage>
- <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">584113</Empennage>
- <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">639568</LandingGear>
- <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">879551</Pylons>
- <PowerUnit Desc="Costs for all installed engines with systems without pylons">
- <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">13337566</PowerUnitTotal>
- <PowerUnitComponents>
- <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">11357394</EquippedEngines>
- <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">1791842</Nacelles>
- <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">107416</BleedAirSystem>
- <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">80914</FuelSystem>
- </PowerUnitComponents>
- </PowerUnit>
- <Systems>
- <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">7436254</SystemsTotal>
- <SystemsComponents>
- <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">273442</APU>
- <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">220982</HydraulicSystem>
- <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">694499</AirConditioning>
- <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">40295</DeIcing>
- <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">39314</FireProtection>
- <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">598096</FlightControls>
- <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">343899</Instruments>
- <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">558835</AutomaticFlightSystem>
- <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">2278329</Navigation>
- <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">1117671</Communication>
- <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">1270893</ElectricalSystem>
- </SystemsComponents>
- </Systems>
- <Furnishings>
- <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">1442699</FurnishingsTotal>
- <FurnishingsComponents>
- <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">1048900</Furnishing>
- <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">41911</FixedEmergencyOxygen>
- <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">228444</Lighting>
- <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">123443</WaterInstallation>
- </FurnishingsComponents>
- </Furnishings>
- <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">1415894</OperatorsItems>
- <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">4665217</FinalAssembly>
- </RCComponents>
- </RecurringCosts>
- <OperatingCosts>
- <OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal">
- <FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">2230</FlightsPerYear>
- <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">1</SeatLoadFactor>
- </OperatingScenario>
- <DirectOperatingCosts>
- <DOC_total Desc="Summe aller DOCComponents (s.u)">
- <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">20437514.98</DOC_year>
- <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7204.76</DOC_FH>
- <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9164.81</DOC_flight>
- <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">9.9</DOC_km>
- <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.6</DOC_100ASK>
- </DOC_total>
- <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
- <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">17054173.5</COC_year>
- <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">6012.05</COC_FH>
- <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">7647.62</COC_flight>
- <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">8.26</COC_km>
- <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">5.50770807</COC_100ASK>
- </COC_total>
- <DOCComponents Desc="DOC-Anteile in 100ASK">
- <Charge Desc="Gebuehren pro 100ASK">
- <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">1.83</ChargeTotal>
- <ChargesComponents>
- <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0.73</NavigationCharge>
- <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0.33</LandingCharge>
- <LandingChargeComponents>
- <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge>
- <NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge>
- <ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0.33</ChargeWithoutEmission>
- </LandingChargeComponents>
- <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0.77</GroundCharge>
- </ChargesComponents>
- </Charge>
- <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0.98</Depreciation>
- <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0.11</Insurance>
- <Maintenance Desc="Wartungskosten">
- <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0.75</MaintenanceTotal>
- <MaintenanceComponents>
- <Airframe Desc="Wartungskosten Airframe">
- <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0.3</AirframeTotal>
- <CostComponents>
- <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.243</LabourCosts>
- <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.061</MaterialCosts>
- </CostComponents>
- <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
- <ATA21 Desc="Environmental Control System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0134</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0107</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0027</MaterialCosts>
- </CostComponents>
- </ATA21>
- <ATA22 Desc="Autoflight">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0127</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0102</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
- </CostComponents>
- </ATA22>
- <ATA23 Desc="Communications">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0123</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0098</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
- </CostComponents>
- </ATA23>
- <ATA24 Desc="Electrical System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0211</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0169</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0042</MaterialCosts>
- </CostComponents>
- </ATA24>
- <ATA25 Desc="Furnishing">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0409</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0327</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0082</MaterialCosts>
- </CostComponents>
- </ATA25>
- <ATA26 Desc="Fire Protection">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0043</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0035</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0009</MaterialCosts>
- </CostComponents>
- </ATA26>
- <ATA27 Desc="Flight Control System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.025</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.02</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.005</MaterialCosts>
- </CostComponents>
- </ATA27>
- <ATA28 Desc="Fuel System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0022</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
- </CostComponents>
- </ATA28>
- <ATA29 Desc="Hydraulic System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0131</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0105</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0026</MaterialCosts>
- </CostComponents>
- </ATA29>
- <ATA30 Desc="Ice and Rain Protection">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
- </CostComponents>
- </ATA30>
- <ATA31 Desc="Instrumentation">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0013</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
- </CostComponents>
- </ATA31>
- <ATA32 Desc="Landing Gear">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0559</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0447</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0112</MaterialCosts>
- </CostComponents>
- </ATA32>
- <ATA33 Desc="Lights">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0051</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0041</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</MaterialCosts>
- </CostComponents>
- </ATA33>
- <ATA34 Desc="Navigation">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0142</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0113</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0028</MaterialCosts>
- </CostComponents>
- </ATA34>
- <ATA35 Desc="Oxygen">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.003</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0006</MaterialCosts>
- </CostComponents>
- </ATA35>
- <ATA36 Desc="Pneumatic">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0036</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0029</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0007</MaterialCosts>
- </CostComponents>
- </ATA36>
- <ATA38 Desc="Water and Waste">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0019</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0005</MaterialCosts>
- </CostComponents>
- </ATA38>
- <ATA49 Desc="APU">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0104</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0083</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0021</MaterialCosts>
- </CostComponents>
- </ATA49>
- <ATA51 Desc="Structure">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.004</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0032</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0008</MaterialCosts>
- </CostComponents>
- </ATA51>
- <ATA52 Desc="Doors">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0054</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0044</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA52>
- <ATA53 Desc="Fuselage">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0057</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA53>
- <ATA54 Desc="Nacelles">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0002</MaterialCosts>
- </CostComponents>
- </ATA54>
- <ATA55 Desc="Stabilizers">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
- </CostComponents>
- </ATA55>
- <ATA56 Desc="Windows">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0081</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0065</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</MaterialCosts>
- </CostComponents>
- </ATA56>
- <ATA57 Desc="Wings">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0056</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA57>
- <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0294</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0235</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0059</MaterialCosts>
- </CostComponents>
- </ATA99>
- </AirframeComponents>
- </Airframe>
- <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0.45</Engine>
- </MaintenanceComponents>
- </Maintenance>
- <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">2.44</Fuel>
- <Crew Desc="Crew Kosten">
- <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0.49</CrewTotal>
- <CrewComponents>
- <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.12</FlightCrew>
- <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.36</CabinCrew>
- </CrewComponents>
- </Crew>
- <Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay>
- </DOCComponents>
- </DirectOperatingCosts>
- <IndirectOperatingCosts>
- <IOC_total Desc="Summe aller IOCComponents (s.u)">
- <IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">20699680.51</IOC_year>
- <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7297.17</IOC_FH>
- <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9282.37</IOC_flight>
- <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">10.02</IOC_km>
- <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.68</IOC_100ASK>
- </IOC_total>
- </IndirectOperatingCosts>
- </OperatingCosts>
- <EndOfLifeCosts>
- <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">48616</EOLCTotal>
- <EOLCTotalComponents>
- <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">9140</TransportToEoLSite>
- <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">124837</DisassemblyAndDismantling>
- <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">-86485</Recycling>
- <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">297</Incineration>
- <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">827</Landfill>
- </EOLCTotalComponents>
- </EndOfLifeCosts>
- </LCC>
- </MonetaryValues>
- <EcologicalValues Desc="Oekologische Bewertung">
- <Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse">
- <NoisePathFiles>
- <Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure>
- <Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach>
- </NoisePathFiles>
- <NoiseCertificationLevels>
- <LateralPoint>
- <LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower>
- <SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </LateralPoint>
- <FlyoverPoint>
- <Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover>
- <SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </FlyoverPoint>
- <ApproachPoint>
- <Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach>
- <SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </ApproachPoint>
- <CumulativeValues>
- <EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB>
- <SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </CumulativeValues>
- </NoiseCertificationLevels>
- <CommunityNoiseLevels>
- <TakeOff>
- <SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL>
- <SPLarea>
- <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
- <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
- </SPLarea>
- <PNLarea>
- <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
- <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
- </PNLarea>
- <PNLTarea>
- <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
- <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
- </PNLTarea>
- <EPNLarea>
- <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
- <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
- </EPNLarea>
- <LoudnessArea>
- <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
- <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
- </LoudnessArea>
- <TonalityArea>
- <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
- <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
- <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
- <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
- </TonalityArea>
- <SharpnessArea>
- <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
- <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
- </SharpnessArea>
- <PsychoacousticAnnoyanceArea>
- <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
- <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
- </PsychoacousticAnnoyanceArea>
- <SELarea Desc="Sound Exposure Level area">
- <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
- <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
- <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
- <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
- </SELarea>
- </TakeOff>
- <Approach>
- <SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL>
- <SPLarea>
- <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
- <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
- </SPLarea>
- <PNLarea>
- <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
- <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
- </PNLarea>
- <PNLTarea>
- <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
- <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
- </PNLTarea>
- <EPNLarea>
- <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
- <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
- </EPNLarea>
- <LoudnessArea>
- <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
- <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
- </LoudnessArea>
- <TonalityArea>
- <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
- <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
- <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
- <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
- </TonalityArea>
- <SharpnessArea>
- <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
- <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
- </SharpnessArea>
- <PsychoacousticAnnoyanceArea>
- <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
- <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
- </PsychoacousticAnnoyanceArea>
- <SELarea Desc="Sound Exposure Level area">
- <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
- <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
- <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
- <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
- </SELarea>
- </Approach>
- <CumulativeValues>
- <EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB>
- <SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </CumulativeValues>
- </CommunityNoiseLevels>
- </Noise>
- <Emissions>
- <Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm">
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">11763648.53</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">40697548.71</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">22681.579</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">506.978</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">10059.553</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">16890.095</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">176.255</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">982.444</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0.019</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">1432.078</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-4663.364</HC>
- </Development>
- <Production>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">618228.677</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">5361791.97</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">1320.026</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">1715.593</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">2280.541</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">1327.591</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">5.711</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-5.298</HC>
- </Production>
- <Operations>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">649479288.1</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">269362047.2</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">821056.648</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">279870.45</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">533623.487</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">749253.374</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">10631.577</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-247022.508</HC>
- <OperationComponents>
- <ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">2844.948</CO2>
- <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">1084.134</H2O>
- <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.759</SO2>
- <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">99.106</HC>
- <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">5.747</CO>
- <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">11.071</NOx>
- <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.023</PM10>
- </ICAO_LTO>
- <Mission Desc="Environmental analysis of one study mission">
- <LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)">
- <Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">19.622</Total>
- <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">14</TaxiTime>
- <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0.311</TakeOffTime>
- <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0.933</ClimbOutTime>
- <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">4.377</ApproachTime>
- </LTOTimes>
- <LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">1500.242</CO2>
- <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">571.702</H2O>
- <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.4</SO2>
- <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">-2.376</HC>
- <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">2.018</CO>
- <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">3.831</NOx>
- <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.009</PM10>
- </LTO>
- <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">9149.073</CO2>
- <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">3486.468</H2O>
- <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">2.441</SO2>
- <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">-2.055</HC>
- <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">1.349</CO>
- <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">7.688</NOx>
- <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0.01</PM10>
- </Cruise>
- </Mission>
- </OperationComponents>
- </Operations>
- <EndOfLife>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">-114694.14</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">-1466106.754</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">-495.854</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">-1949.608</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">-1061.466</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">-304.18</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0.419</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-3.735</HC>
- </EndOfLife>
- </Emissions>
- <CED Desc="Cumulative Energy Demand">
- <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">1.033604491e+16</CEDTotal>
- <CEDComponents>
- <Development Desc="Development" ToolLevel="1" Unit="MJ">2.115958924e+14</Development>
- <Production Desc="Production" ToolLevel="1" Unit="MJ">1.332765215e+13</Production>
- <Operations Desc="Operation" ToolLevel="1" Unit="MJ">1.011292433e+16</Operations>
- <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">-1.802957726e+12</EndOfLife>
- </CEDComponents>
- </CED>
- <ClimateImpact Desc="Climate Impact due to Aircraft Operation">
- <ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0.0014420111</ATR>
- <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">2.13271e-05</AGTP>
- <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">3.52252e-05</AGTP100>
- <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">4.29914e-05</AGWP>
- <AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100>
- </ClimateImpact>
- <AirQuality Desc="Climate Impact due to Aircraft Operation">
- <ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-">
- <HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">-0.4355</HC>
- <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0.0614</CO>
- <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0.1915</NOx>
- <soot Desc="TF Russ" ToolLevel="1" Unit="-">0.0767</soot>
- </ToleranceFactors>
- <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">-0.0265</AirQualityIndex>
- </AirQuality>
- </EcologicalValues>
- <Requirements Desc="Designforderungen">
- <m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload>
- <m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload>
- <DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
- <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
- <TOFL_Design Desc="Auslegungsstartstrecke (Balanced Field Length)" Unit="m">2200</TOFL_Design>
- <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+10)" Unit="min">35</TTC_Design>
- <ClimbGradients Desc="Steiggradientenforderungen">
- <secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment>
- <finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment>
- <approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO>
- <approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI>
- </ClimbGradients>
- <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
- <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
- </ClimbSpeedSchedule>
- <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- </DescentSpeedSchedule>
- <h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design>
- <M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design>
- <LDN_Design Desc="Auslegungslandestrecke (Sicherheitslandestrecke)" Unit="m">1850</LDN_Design>
- <V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design>
- <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
- <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
- <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
- <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
- <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
- </DesignMission>
- <StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
- <R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design>
- <m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload>
- <NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX>
- <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
- <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
- </ClimbSpeedSchedule>
- <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- </DescentSpeedSchedule>
- <h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise>
- <M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise>
- <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
- <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
- <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
- <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
- <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
- </StudyMission>
- <FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod>
- <V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed>
- <DesignFlightEnvelope>
- <VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO>
- <MMO Desc="Max operating Mach No." Unit="-">0.82</MMO>
- <h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating>
- <h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI>
- </DesignFlightEnvelope>
- <SizeLimits Desc="maximale geometrische Abmasse">
- <SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit>
- </SizeLimits>
- <ACN Desc="Aircraft Classification Number">
- <ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType>
- <ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory>
- <ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit>
- </ACN>
- </Requirements>
- <DesignSpecification Desc="Spezifikation des Entwurfs">
- <Configuration Desc="Qualitative Beschreibung der Konfiguration">
- <Wing Desc="Parameter des Fluegels">
- <Position Desc="Fluegellage low, mid, high" Unit="-">low</Position>
- </Wing>
- <Stabiliser Desc="Parameter des Hoehenleitwerks">
- <h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing>
- </Stabiliser>
- <LandingGear Desc="Fahrwerksanordnung">
- <MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition>
- <Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable>
- </LandingGear>
- <Fuselage Desc="Fuselage parameters">
- <Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized>
- </Fuselage>
- <CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType>
- <Fin Desc="Parameter des Seitenleitwerks">
- <FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig>
- </Fin>
- </Configuration>
- <Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen">
- <MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX>
- <PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks>
- <PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1">
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">33</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats>
- </Class>
- </PAXDeck>
- </Accommodation>
- <Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs">
- <CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks>
- <CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1">
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs>
- </ULDType>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs>
- </ULDType>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs>
- </ULDType>
- </Compartment>
- </CargoDeck>
- </Cargo>
- <Propulsion Desc="Vorgaben zum Antriebssystem">
- <TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine>
- <NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines>
- <PositionOfEngines Desc="Positionierung der Triebwerke">
- <EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing>
- <EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage>
- <EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage>
- <WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition>
- </PositionOfEngines>
- <FuelDensity Desc="Dichte des Kraftstoffs" Unit="kg/l">0.785</FuelDensity>
- </Propulsion>
- <TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks">
- <NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks>
- <NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks>
- <NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks>
- </TankConfiguration>
- <HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem">
- <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.3</C_LmaxT-O>
- <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding>
- </HighLiftSystem>
- <DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen">
- <n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1>
- <n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2>
- </DesignLoads>
- <Technology Desc="Vorgaben spezieller Technologien">
- <LaminarFlow Desc="HLFC oder NLF">
- <Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird">
- <Wing>
- <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
- <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
- </Wing>
- <Stabilizer>
- <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
- <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
- </Stabilizer>
- <Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin>
- <Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles>
- </Components>
- </LaminarFlow>
- <ElectricTaxiing>
- <DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing>
- <EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime>
- </ElectricTaxiing>
- <BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem>
- </Technology>
- </DesignSpecification>
-</AcftExchangeFile>
diff --git a/projects/reporting/reportHTML/ReportXYZ.html b/projects/reporting/reportHTML/ReportXYZ.html
new file mode 100644
index 0000000000000000000000000000000000000000..dbd870dcbffa1953060c9f89e1aa692a64dfa3aa
--- /dev/null
+++ b/projects/reporting/reportHTML/ReportXYZ.html
@@ -0,0 +1,135 @@
+<?xml version="1.0" encoding="utf-8"?>
+<html lang="en">
+ <head>
+ <meta content="width=device-width, initial-scale=1.0" name="viewport" charset="utf-8"/>
+ <title><probably same as report name></title>
+ <link href="style.css" rel="stylesheet"/>
+ </head>
+ <body>
+ <div class="content">
+ <h1>Report - <some name></h1>
+ <div class="container">
+ <div class="box data">
+ <h2>CSR nr1</h2>
+ <table class="content-table">
+ <caption>Residual Values</caption>
+ <thead>
+ <tr>
+ <th>paramter</th>
+ <th>value</th>
+ <th>unit</th>
+ </tr>
+ </thead>
+ <tbody>
+ <tr>
+ <td>MTOM</td>
+ <td>1223.25</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Moment of Inertia</td>
+ <td>0.80000000004656613</td>
+ <td>kgm^2</td>
+ </tr>
+ <tr>
+ <td>OME</td>
+ <td>39544.5</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Some Name</td>
+ <td>-888</td>
+ <td>1</td>
+ </tr>
+ <tr>
+ <td>Another Name</td>
+ <td>-999</td>
+ <td>1</td>
+ </tr>
+ </tbody>
+ </table>
+ </div>
+ <div class="box data">
+ <h2>CSR nr2</h2>
+ <table class="content-table">
+ <caption>Residual Values</caption>
+ <thead>
+ <tr>
+ <th>paramter</th>
+ <th>value</th>
+ <th>unit</th>
+ </tr>
+ </thead>
+ <tbody>
+ <tr>
+ <td>MTOM</td>
+ <td>-266344.75</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Moment of Inertia</td>
+ <td>100000.80000000005</td>
+ <td>kgm^2</td>
+ </tr>
+ <tr>
+ <td>OME</td>
+ <td>-713755.5</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Some Name</td>
+ <td>-888</td>
+ <td>1</td>
+ </tr>
+ <tr>
+ <td>Another Name</td>
+ <td>-123</td>
+ <td>1</td>
+ </tr>
+ </tbody>
+ </table>
+ </div>
+ <div class="box data">
+ <h2>CSR nr3</h2>
+ <table class="content-table">
+ <caption>Residual Values</caption>
+ <thead>
+ <tr>
+ <th>paramter</th>
+ <th>value</th>
+ <th>unit</th>
+ </tr>
+ </thead>
+ <tbody>
+ <tr>
+ <td>MTOM</td>
+ <td>75791.25</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Moment of Inertia</td>
+ <td>-10140.199999999953</td>
+ <td>kgm^2</td>
+ </tr>
+ <tr>
+ <td>OME</td>
+ <td>43000.5</td>
+ <td>kg</td>
+ </tr>
+ <tr>
+ <td>Some Name</td>
+ <td>-888</td>
+ <td>1</td>
+ </tr>
+ <tr>
+ <td>Another Name</td>
+ <td>-9999</td>
+ <td>1</td>
+ </tr>
+ </tbody>
+ </table>
+ </div>
+ </div>
+ </div>
+ </body>
+</html>
diff --git a/projects/reporting/reportHTML/style.css b/projects/reporting/reportHTML/style.css
new file mode 100644
index 0000000000000000000000000000000000000000..4030d8e5b21256094f5254bdfc2b30401c0fcc97
--- /dev/null
+++ b/projects/reporting/reportHTML/style.css
@@ -0,0 +1,178 @@
+
+*, *:before, *:after {
+ margin: 0;
+ padding: 0;
+ box-sizing: border-box;
+}
+html, body {
+ background-color: #2a2d33;
+ font-family: system-ui, sans-serif;
+ font-size: 1.3rem;
+ color: #2c3e50;
+ line-height: 1.3;
+ background-size: cover;
+}
+
+table {
+ margin-left: 0;
+ margin-right: auto;
+}
+
+.logo {
+ background-image: url('logoUNICADO_icon.svg');
+ height: 75vh;
+ width: 100%;
+ opacity: 0.2;
+ filter: grayscale(100%);
+ background-size: contain;
+ background-repeat: no-repeat;
+ background-position: center center;
+ position: relative center;
+
+}
+
+.content {
+ position: absolute;
+ width: 98%;
+ height: 85%;
+ top: 0rem;
+ left: 1rem;
+ padding-left: 0rem;
+ box-sizing: border-box;
+ min-width: fit-content;
+
+}
+
+.content h1 {
+ color: #ecf0f1;
+ margin: 1rem 0.1rem;
+ font-size: 2.7rem;
+ font-weight: lighter;
+ font-variant: small-caps;
+}
+
+.container {
+ position: absolute;
+ display: flex;
+ width: 100%;
+ height: 100%;
+}
+
+
+.box {
+ width: 50%;
+ overflow-y: auto;
+ overflow-x: auto;
+ scrollbar-width: none;
+ scrollbar-color: #f0f0f0 #f0f0f0;
+ padding: 0;
+ margin-right: 0.2rem;
+ background-color: #ecf0f1;
+ box-shadow: 5px 5px 5px black;
+ border-radius: 0.5rem;
+ min-width: fit-content;
+ text-align: center;
+}
+
+
+.data {
+ background-color: #ecf0f1;
+ padding: auto;
+ min-width: fit-content;
+ max-width: 50%;
+}
+
+.plot {
+ background-color: #ecf0f1;
+ text-align: center;
+ max-width: 50%;
+}
+
+.box h2 {
+ margin-left: 0.5rem;
+ font-weight: normal;
+ font-variant: small-caps;
+ font-size: 1.5rem;
+ text-align: left;
+}
+
+.box h3 {
+ margin-left: 0.5rem;
+ font-weight: normal;
+ font-variant: small-caps;
+ font-size: 1.2rem;
+ text-align: left;
+}
+
+.box h4 {
+ margin-left: 0.5rem;
+ font-weight: normal;
+ font-variant: small-caps;
+ font-size: 1.0rem;
+ text-align: left;
+}
+
+.box ul {
+ list-style-type: disc;
+ margin-left: 0rem;
+ padding-left: 2rem;
+ text-align: left;
+}
+
+.box ul li {
+ margin: 0 0 0 0;
+ padding-left: 0;
+ font-size: 0.9rem;
+ font-weight: lighter;
+}
+
+.content-table {
+ margin-left: 2rem;
+ padding: 0.50rem;
+ font-size:0.9rem;
+ flex-basis: 100rem;
+ font-weight: lighter;
+ padding-bottom: 2rem;
+}
+
+.content-table caption {
+ text-align: left;
+ font-weight:600;
+ font-size: larger;
+ font-variant: small-caps;
+}
+
+.content-table th {
+ text-align: left;
+ padding-right: 1rem;
+ white-space: nowrap;
+ min-width: 3rem;
+ font-weight: normal;
+}
+
+.content-table td {
+ padding-right: 1rem;
+ text-align: left;
+}
+
+.content-table td.row-header {
+ font-weight: normal;
+ text-align: left;
+ padding-right: 0.5rem;
+}
+
+.content-table td.content-data-number {
+ text-align: right;
+}
+
+.content-table tbody tr:hover {
+ color: #ee5253;
+ cursor: pointer;
+}
+
+.plot img.image-plot {
+ min-width: none;
+ width: 90%;
+ color: #ecf0f1;
+
+}
diff --git a/test-upstream-files/newFormat-CSMR-2020.xml b/test-upstream-files/newFormat-CSMR-2020.xml
index e3c71f976f590f22df233ef3c502842915ae3a1b..d0768124788815230fa486f872e83b5f3a65a196 100644
--- a/test-upstream-files/newFormat-CSMR-2020.xml
+++ b/test-upstream-files/newFormat-CSMR-2020.xml
@@ -794,7 +794,7 @@
<mass_properties description="maximum takeoff mass properties">
<inertia description="Inertia with regard to the total center of gravity.">
<j_xx description="Inertia in x.">
- <value>1510141.8121567257</value>
+ <value>1500000.80</value>
<unit>kgm^2</unit>
<lower_boundary>-inf</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -869,7 +869,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>79002.14738244547</value>
+ <value>79000.25</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
@@ -955,7 +955,7 @@
</z>
</center_of_gravity>
<mass description="Mass">
- <value>42929.835124</value>
+ <value>43000.50</value>
<unit>kg</unit>
<lower_boundary>0</lower_boundary>
<upper_boundary>inf</upper_boundary>
diff --git a/test-upstream-files/oldFormat-CSR.xml b/test-upstream-files/oldFormat-CSR.xml
deleted file mode 100644
index 32bba1c26e51b537fc1e04894fd0a3df65a7e46c..0000000000000000000000000000000000000000
--- a/test-upstream-files/oldFormat-CSR.xml
+++ /dev/null
@@ -1,3866 +0,0 @@
-<AcftExchangeFile>
- <General Desc="Allgemeine Angaben">
- <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
- <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-01</Model>
- </General>
- <MassesAndLoadings Desc="-">
- <MassBreakdown Desc="Massenverteilung">
- <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
- <Mass ToolLevel="1" Unit="kg">8535.455741</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4">
- <Mass ToolLevel="1" Unit="kg">6278.799947</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor>
- <EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor>
- <EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor>
- </CenterWing>
- <WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8">
- <Mass ToolLevel="1" Unit="kg">2256.655794</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
- <Mass ToolLevel="1" Unit="kg">291.6450898</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FixedLeadingEdge>
- <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
- <Mass ToolLevel="1" Unit="kg">373.9546469</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </MovableLeadingEdge>
- <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
- <Mass ToolLevel="1" Unit="kg">582.2672595</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FixedTrailingEdge>
- <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
- <Mass ToolLevel="1" Unit="kg">1008.788798</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </MovableTrailingEdge>
- </WingLEandTE>
- <Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9">
- <Mass ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </Miscellaneous>
- </Wing>
- <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
- <Mass Desc="-" ToolLevel="1" Unit="kg">8888.102165</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Fuselage>
- <Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements">
- <Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1257.118042</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.40806564</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- <Tailplane Desc="Airbus Chapter 13">
- <Mass ToolLevel="1" Unit="kg">705.5278242</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.73963722</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- </Tailplane>
- <Fin Desc="Airbus Chapter 14">
- <Mass Desc="-" ToolLevel="1" Unit="kg">551.5902181</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">32.98395918</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
- </RefPoint>
- </Fin>
- </Empennage>
- <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2518.773274</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.32982807</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.469648031</h_Item>
- </RefPoint>
- <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">377.8159911</TotalMass>
- <RefPoint Desc="Position of NoseGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
- <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
- <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
- <RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
- <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
- <RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Strut>
- <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
- <RefPoint Desc="position of strut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Strut>
- <SupportStrut>
- <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
- <RefPoint Desc="position of suppStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SupportStrut>
- <WheelGroupConnection>
- <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
- <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
- <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WheelGroupConnection>
- <WheelGroup>
- <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
- <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
- <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
- <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
- </WheelGroup>
- </Gear>
- </LandingGear>
- <Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1049.543431</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.59758377</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.838904205</h_Item>
- </RefPoint>
- </Pylons>
- <PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit">
- <Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">7983.304178</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.56488425</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.882731847</h_Item>
- </RefPoint>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
- <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2237.636365</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2">
- <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2237.636365</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <EngineDry Desc="Engine dry mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineDry>
- <Nacelle Desc="Nacelle mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Nacelle>
- <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OtherSystems>
- <Prop Desc="Propeller mass">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Prop>
- </Engine>
- <BleedAirSystem Desc="Airbus Chapter 21, ATA36">
- <Mass Desc="-" ToolLevel="1" Unit="kg">170.4663501</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </BleedAirSystem>
- <EngineControls Desc="Airbus Chapter 22">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </EngineControls>
- <FuelSystem Desc="Airbus Chapter 25, ATA28">
- <Mass Desc="-" ToolLevel="1" Unit="kg">313.2402355</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
- </RefPoint>
- </FuelSystem>
- </PowerUnit>
- <Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
- <Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5309.46001</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.22640698</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-0.5973844066</h_Item>
- </RefPoint>
- <APU Desc="Airbus Chapter 30, ATA49">
- <Mass Desc="-" ToolLevel="1" Unit="kg">269.6524446</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">35.12321805</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </APU>
- <HydraulicGeneration Desc="Airbus Chapter 31, ATA 29">
- <Mass Desc="-" ToolLevel="1" Unit="kg">177.4943728</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </HydraulicGeneration>
- <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
- <Mass Desc="-" ToolLevel="1" Unit="kg">795.934215</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </HydraulicDistribution>
- <AirConditioning Desc="Airbus Chapter 33, ATA21">
- <Mass Desc="-" ToolLevel="1" Unit="kg">711.2165166</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- </AirConditioning>
- <DeIcing Desc="Airbus Chapter 34, ATA30">
- <Mass Desc="-" ToolLevel="1" Unit="kg">41.98276817</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </DeIcing>
- <FireProtection Desc="Airbus Chapter 35, ATA26">
- <Mass Desc="-" ToolLevel="1" Unit="kg">92.36094204</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </FireProtection>
- <FlightControls Desc="Airbus Chapter 36, ATA27">
- <Mass Desc="-" ToolLevel="1" Unit="kg">699.137886</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
- </RefPoint>
- <Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
- <Mass Desc="-" ToolLevel="1" Unit="kg">42.43977661</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Roll>
- <Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1">
- <Mass Desc="-" ToolLevel="1" Unit="kg">97.75474213</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Yaw>
- <Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2">
- <Mass Desc="-" ToolLevel="1" Unit="kg">30.4466164</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Pitch>
- <MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3">
- <Mass Desc="-" ToolLevel="1" Unit="kg">63.38988998</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </MovableHorizontalTail>
- <Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4">
- <Mass Desc="-" ToolLevel="1" Unit="kg">143.8595475</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Flaps>
- <SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.5">
- <Mass Desc="-" ToolLevel="1" Unit="kg">38.76193929</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </SpoilersAirbrakesLiftdumpers>
- <Slats Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.6">
- <Mass Desc="-" ToolLevel="1" Unit="kg">142.6577969</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Slats>
- <CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7">
- <Mass Desc="-" ToolLevel="1" Unit="kg">139.8275772</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </CommonInstallation>
- </FlightControls>
- <Instruments Desc="Airbus Chapter 37, ATA31">
- <Mass ToolLevel="1" Unit="kg">85.16128872</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.34075992</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Instruments>
- <AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22">
- <Mass ToolLevel="1" Unit="kg">138.3870942</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </AutomaticFlightSystem>
- <Navigation Desc="Airbus Chapter 39, ATA34">
- <Mass Desc="-" ToolLevel="1" Unit="kg">564.1935378</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Navigation>
- <Communication Desc="Airbus Chapter 40, ATA23">
- <Mass Desc="-" ToolLevel="1" Unit="kg">276.7741884</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Communication>
- <ElectricalGeneration Desc="Airbus Chapter 41, ATA24">
- <Mass Desc="-" ToolLevel="1" Unit="kg">774.2507101</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </ElectricalGeneration>
- <ElectricalDistribution Desc="Airbus Chapter 42, ATA24">
- <Mass Desc="-" ToolLevel="1" Unit="kg">682.914046</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </ElectricalDistribution>
- </Systems>
- <Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings">
- <Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3114.623325</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <Furnishing Desc="Airbus Chapter 50, ATA25">
- <Mass Desc="-" ToolLevel="1" Unit="kg">2464.223172</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Furnishing>
- <FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35">
- <Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </FixedEmergencyOxygen>
- <Lighting Desc="Airbus Chapter 52, ATA33">
- <Mass Desc="-" ToolLevel="1" Unit="kg">261.9261532</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </Lighting>
- <WaterInstallation Desc="Airbus Chapter 53, ATA38">
- <Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </WaterInstallation>
- </Furnishings>
- <OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items">
- <Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3326.415065</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.54754916</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- <OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1575.865065</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.5703719</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OperatorEquipment>
- <OperationalEquipment Desc="Airbus Chapter 61 (movable equipment)">
- <Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.72658107</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </OperationalEquipment>
- </OperatorsItems>
- <NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements">
- <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
- <RefPoint Desc="position of mass item to global point of reference">
- <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
- <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
- <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
- </RefPoint>
- </NotAllocated>
- </MassBreakdown>
- <MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM>
- <MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">65025.01668</MLM>
- <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">76962.57512</MTOM>
- <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
- <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38656.38017</MME>
- <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">41982.79523</OME>
- <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">61982.79523</MZFM>
- <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
- <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">31084.34394</MaximumUsableFuel>
- <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">628.681385</WingLoading>
- <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3218120393</ThrustToWeight>
- <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
- <MomentsOfInertia Desc="Flaechentraegheitsmomente">
- <Ixx Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixx>
- <Iyy Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyy>
- <Izz Desc="-" ToolLevel="1" Unit="kg*m2">0</Izz>
- <Ixy Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixy>
- <Ixz Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixz>
- <Iyz Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyz>
- </MomentsOfInertia>
- <CentreOfGravityRange Desc="Schwerpunktsgrenzen">
- <TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7359472859</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.56950713</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </TrimRefPt>
- <ForwardLimit Desc="Vorderste Schwerpunktlage">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9505895064</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.4584795</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </ForwardLimit>
- <AftLimit Desc="Hinterste Schwerpunktlage">
- <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-1.011726725</h>
- <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.65854294</r>
- <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
- </AftLimit>
- </CentreOfGravityRange>
- </MassesAndLoadings>
- <Geometry Desc="Geometriebeschreibung">
- <UsedElements Desc="Liste der verwendeten Geometrieelemente">
- <LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces>
- <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface>
- <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface>
- <VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces>
- <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface>
- <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface>
- <Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages>
- <Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage>
- <Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle>
- <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle>
- <Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon>
- <Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon>
- <Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear>
- <Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear>
- </UsedElements>
- <LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing">
- <SurfaceRefPoint Desc="position of wing to global point of reference">
- <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Surface>
- <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of lifting surface geometry">
- <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
- <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
- <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface>
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints>
- <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_15.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">6.969546741</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.363049953</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.115537999</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_11.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.363049953</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.036840684</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">11.93625533</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2062430536</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- </SurfaceParameters>
- </LiftingSurface>
- <LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser">
- <SurfaceRefPoint Desc="position of wing to global point of reference">
- <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.1606612</r_Surface>
- <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of lifting surface geometry">
- <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
- <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
- <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.140234056</i_Surface>
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.962556849</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.11563951</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.392179667</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
- <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
- <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </HalfSurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
- <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
- <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
- <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
- </DeflectionAngle>
- </LEDevice>
- </ControlDeviceSetup>
- </HalfSurfaceDescription>
- </SurfaceParameters>
- </LiftingSurface>
- <VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin">
- <SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.20843962</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.692105859</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of vertical surface geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.914778427</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.564960467</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">7.105751949</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
- <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
- <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
- <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
- <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
- </SurfaceSegment>
- <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
- <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
- <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
- <Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type>
- <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
- <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
- <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
- <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
- <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
- <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
- <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
- </DeflectionAngle>
- </TEDevice>
- </ControlDeviceSetup>
- </SurfaceParameters>
- </VerticalSurface>
- <Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage">
- <FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference">
- <r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage>
- <y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage>
- <h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage>
- </FuselageRefPoint>
- <FuselageParameters Desc="parametric description of the fuselage">
- <NoseDescription>
- <NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments>
- <TipSegment>
- <h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5351396212</h_Tip>
- </TipSegment>
- <NoseSegment ID="1">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6205763694</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.6626671728</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06782437376</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5351396212</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="2">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.229534829</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.312928447</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.2034731213</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4376004301</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="3">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.814885649</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.937980885</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3391218688</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3438425644</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="4">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.363843474</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.524171961</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4747706164</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2559139029</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="5">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.862283086</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.05641841</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.6104193639</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1760769356</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="6">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.293963779</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.517377993</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7460681114</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1069329983</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="7">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.639314251</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.886151978</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.8817168589</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05161690045</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="8">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.873337327</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136047749</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.017365606</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01413253478</deltah_Segment>
- </NoseSegment>
- <NoseSegment ID="9">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
- <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment>
- <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.153014354</l_Segment>
- <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment>
- </NoseSegment>
- </NoseDescription>
- <MidSectionDescription>
- <MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments>
- <MidSectionSegment ID="1">
- <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
- <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
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- </Fuselage>
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- <NacelleParameters Desc="parametric description of the nacelle">
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- <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData>
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- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
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- <Nacelle Desc="Beschreibung der inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle">
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- </NacelleParameters>
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- <Nacelle Desc="Beschreibung der aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle">
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- </InletSegment>
- <NacelleSegment ID="1">
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- </ExitSegment>
- </NacelleParameters>
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- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
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- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
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- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
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- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
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- <ExitSegment>
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- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Nacelle Desc="Beschreibung der rechten Hecktriebwerksgondel" ID="RightFuselageNacelle">
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- <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
- </NacelleRefPoint>
- <NacelleParameters Desc="parametric description of the nacelle">
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- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
- <InletSegment>
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- <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
- <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <NacelleSegment ID="2">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <ExitSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle">
- <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
- <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
- <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
- </NacelleRefPoint>
- <NacelleParameters Desc="parametric description of the nacelle">
- <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
- <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
- <InletSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
- <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <NacelleSegment ID="2">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <ExitSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle">
- <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
- <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
- <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
- <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
- </NacelleRefPoint>
- <NacelleParameters Desc="parametric description of the nacelle">
- <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
- <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
- <Segments Desc="No of segments" ToolLevel="1">0</Segments>
- <InletSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
- <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
- <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
- </InletSegment>
- <NacelleSegment ID="1">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <NacelleSegment ID="2">
- <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
- <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
- <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
- <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
- <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
- <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
- <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
- </NacelleSegment>
- <ExitSegment>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
- <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
- </ExitSegment>
- </NacelleParameters>
- <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
- </Nacelle>
- <Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.219203967</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.219203967</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon">
- <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
- <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
- <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
- <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
- </SurfaceRefPoint>
- <SurfaceParameters Desc="Parametric description of pylon geometry">
- <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
- <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
- <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
- <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
- <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
- <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
- <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
- <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
- <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
- <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
- </SurfaceSegment>
- </SurfaceParameters>
- </Pylon>
- <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.023847396</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.834540304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
- </Wheel>
- </Gear>
- <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
- <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
- <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
- <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
- <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
- </GearRefPoint>
- <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
- <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
- <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
- <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
- </WheelGroupRefPoint>
- <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
- <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
- <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
- <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
- <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
- <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
- </HingeAxis>
- <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
- <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
- <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
- <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
- <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
- <Wheel Desc="Beschreibung des Rades">
- <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
- <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
- <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
- </Wheel>
- </Gear>
- </Geometry>
- <Structure Desc="Strukturdaten"></Structure>
- <Accommodation Desc="Kabineneinrichtung">
- <PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal>
- <FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew>
- <CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew>
- <Seats Desc="Description of seats">
- <NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">5</NoOfSeatTypes>
- <seat Desc="Description of seat" ID="1">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">commuter</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">1</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="5">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="2">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="3">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">GeneralAviation</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25.1</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="4">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- <seat Desc="Description of seat" ID="5">
- <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">first</seatClassType>
- <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">21.25</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">42.5</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
- </seatConfiguration>
- <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
- <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
- <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
- </seatConfiguration>
- <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
- <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
- </seat>
- </Seats>
- <Galleys Desc="Description of galleys">
- <NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes>
- <Gal Desc="Description of galley" ID="1">
- <nameGalley Desc="Name of galley" ToolLevel="1">large_galley</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power>
- </Gal>
- <Gal Desc="Description of galley" ID="2">
- <nameGalley Desc="Name of galley" ToolLevel="1">small_galley</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power>
- </Gal>
- <Gal Desc="Description of galley" ID="3">
- <nameGalley Desc="Name of galley" ToolLevel="1">0</nameGalley>
- <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">0</NumberOfGalleys>
- <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">0</mass>
- <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">0</power>
- </Gal>
- </Galleys>
- <Lavatories Desc="Description of lavatories">
- <NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes>
- <Lav Desc="Description of lavatory" ID="1">
- <nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory>
- <NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories>
- <mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass>
- </Lav>
- </Lavatories>
- <Cabin Desc="Beschreibung der Kabine">
- <V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">190.47918</V_AirConditioned>
- <CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks>
- <CabinDeck Desc="Parameter eines Kabinendecks" ID="1">
- <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">95.53300238</A_CabinDeck>
- <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
- <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.613074406</w_CabinDeck>
- <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.44091752</l_CabinDeck>
- <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">185.9285625</V_CabinDeck>
- <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck>
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">6.044387137</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.2648459</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- </CabinDeck>
- <CabinDeck Desc="Parameter eines Kabinendecks" ID="2">
- <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">0</A_CabinDeck>
- <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">0</h_CabinDeck>
- <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">0</w_CabinDeck>
- <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">0</l_CabinDeck>
- <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">0</V_CabinDeck>
- <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">0</PAX_CabinDeck>
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">0</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Class>
- </CabinDeck>
- </Cabin>
- <Cargo Desc="Beschreibung des Frachtraums">
- <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">33.22757663</V_Cargo>
- <CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks>
- <CargoDeck Desc="Parameter eines Frachtdecks" ID="1">
- <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">55.02284727</A_CargoDeck>
- <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
- <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.252922327</w_CargoDeck>
- <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">16.91489736</l_CargoDeck>
- <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">34.30498624</V_CargoDeck>
- <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.17849076</V_BulkCargo>
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.69</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.22</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">23.42652858</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- </CargoDeck>
- <CargoDeck Desc="Parameter eines Frachtdecks" ID="2">
- <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">0</A_CargoDeck>
- <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">0</h_CargoDeck>
- <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">0</w_CargoDeck>
- <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">0</l_CargoDeck>
- <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">0</V_CargoDeck>
- <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">0</V_BulkCargo>
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">0</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
- <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
- </Compartment>
- </CargoDeck>
- </Cargo>
- </Accommodation>
- <Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)">
- <NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes>
- <Engine Desc="Triebwerks-/Motortyp" ID="1">
- <TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine>
- <EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel>
- <NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines>
- <ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.039876757</ScaleEngines>
- <ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow>
- <EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">V2527-A5/V2527-A5.xml</EngineDataFile>
- <JetEngineData Desc="Jet spezifische Triebwerksdaten">
- <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">121.4507148</SeaLevelStaticThrust>
- <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.613</FanDiameter>
- </JetEngineData>
- <TurbopropEngineData Desc="Prop spezifische Triebwerksdaten">
- <Prop Desc="Propellerdaten">
- <PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter>
- <PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades>
- <SegmentPointData ToolLevel="1">0</SegmentPointData>
- <Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch>
- <Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness>
- </Prop>
- <P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp>
- </TurbopropEngineData>
- <EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk">
- <w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.829</w_Engine>
- <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.118</h_Engine>
- <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.508</l_Engine>
- </EngineDimensions>
- <NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0">
- <InnerNacelle>
- <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
- <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
- <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
- <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
- <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
- <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
- </InnerNacelle>
- <OuterNacelle>
- <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
- <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
- <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
- <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
- <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
- <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
- </OuterNacelle>
- </NacelleRescaling>
- <ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks">
- <EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+15, SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">121.6192213</EquivalentThrust>
- <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">121.4507148</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.255306839</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01033593619</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.027199488</N1>
- </MaximumTakeOff>
- <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">97.29537705</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.274976051</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01310417914</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.02423458</N1>
- </MaximumGoAround>
- <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+0 bei" Mach="0.78">
- <MaxThrust Desc="Without Offtakes">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">35.65209987</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.6237266005</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01749480683</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1</N1>
- </MaxThrust>
- <BucketThrust Desc="Without Offtakes">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.92001194</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4343473894</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01675722181</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.875</N1>
- </BucketThrust>
- <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
- <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.97268447</Thrust>
- <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4521939534</FuelFlow>
- <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01741036641</TSFC>
- <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.905</N1>
- </BucketThrustOfftakes>
- </MaximumContinous>
- </ScaledPerformanceCharacteristics>
- <UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird">
- <UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines>
- <NacelleID ID="1" ToolLevel="1">0</NacelleID>
- <NacelleID ID="2" ToolLevel="1">0</NacelleID>
- <NacelleID ID="3" ToolLevel="1">0</NacelleID>
- <NacelleID ID="4" ToolLevel="1">0</NacelleID>
- </UsedForNacelles>
- </Engine>
- </Propulsion>
- <Systems>
- <FuelTank Desc="Tank system Parameters">
- <CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks>
- <CentreTank Desc="Center-Tank Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83307738</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330577781</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">10165.96362</TankVolume>
- </CentreTank>
- <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
- <WingTank Desc="Fluegeltank-Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">6.308425637</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
- </WingTank>
- <WingTank Desc="Fluegeltank-Beschreibung" ID="2">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">-6.308425637</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
- </WingTank>
- <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
- <TrimTank Desc="Trimmtank-Beschreibung" ID="1">
- <RefPoint Desc="position of tank reference point in relation to global point of reference">
- <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Tank>
- <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
- <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">0</h_Tank>
- </RefPoint>
- <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">0</TankVolume>
- </TrimTank>
- <TotalFuelVolume Desc="Gesamtes Kraftstoffvolumen aller Tanks" ToolLevel="1" Unit="l">39597.89037</TotalFuelVolume>
- </FuelTank>
- <ATA21_EnvironmentalControlSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.96155032</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.315916839</BleedAir>
- </DesignPower>
- <AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax>
- <Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation>
- </ATA21_EnvironmentalControlSystem>
- <ATA22_AutoFlight>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA22_AutoFlight>
- <ATA23_Communication>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA23_Communication>
- <ATA24_ElectricSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA24_ElectricSystem>
- <ATA25_Furnishing>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA25_Furnishing>
- <ATA26_FireProtection>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA26_FireProtection>
- <ATA27_FlightControlSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">95.17958985</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA27_FlightControlSystem>
- <ATA28_FuelSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">11.89508876</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA28_FuelSystem>
- <ATA29_HydraulicSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.171489811</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- <Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure>
- </ATA29_HydraulicSystem>
- <ATA30_IceRainProtection>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.128183366</BleedAir>
- </DesignPower>
- </ATA30_IceRainProtection>
- <ATA31_Instrumentation>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA31_Instrumentation>
- <ATA32_LandingGear>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">67.03267969</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA32_LandingGear>
- <ATA33_Lights>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.96874401</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA33_Lights>
- <ATA34_Navigation>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA34_Navigation>
- <ATA35_Oxygen>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
- </DesignPower>
- </ATA35_Oxygen>
- <ATA36_BleedAir>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1286368529</BleedAir>
- </DesignPower>
- </ATA36_BleedAir>
- <ATA49_APU>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir>
- </DesignPower>
- </ATA49_APU>
- <ATA70_PropulsionSystem>
- <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
- <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-142.0813445</Electric>
- <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-174.2129642</Hydraulic>
- <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.708144271</BleedAir>
- </DesignPower>
- </ATA70_PropulsionSystem>
- </Systems>
- <Aerodynamics Desc="Aerodynamik">
- <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">17.07161371</LoverD_Cruise>
- <LiftCoefficients Desc="Auftriebsbeiwerte">
- <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5388392246</C_L_design>
- <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.910828613</C_LmaxLanding>
- <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.511580029</C_LmaxT-O>
- <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.534</C_LoptimumCruise>
- <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.56482909</C_L_opt_wing>
- <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03082906473</C_L_opt_stab>
- <C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll>
- </LiftCoefficients>
- <DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)">
- <C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03127999549</C_D_total>
- <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.01011147857</C_D_ind>
- <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
- <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01998021606</C_D_visc_total>
- <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.006065898162</C_D_visc_wing>
- <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001539217794</C_D_visc_stab>
- <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001759127689</C_D_visc_fin>
- <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006881721154</C_D_visc_fus>
- <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001626766969</C_D_visc_nac>
- <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.002107484288</C_D_visc_misc>
- </C_D_visc>
- <C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-">
- <C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_total>
- <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_wing>
- <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0</C_D_wave_stab>
- </C_D_wave>
- <EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor>
- </DragCoefficients>
- <MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)">
- <C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">-0.001284519415</C_M_total>
- </MomentCoefficients>
- <Polar Desc="Flugzeugpolare">
- <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">CSR_polar.xml</PolarFile>
- <Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration>
- <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration>
- </Polar>
- <ReferenceValues Desc="Aerodynamische Bezugsgroessen">
- <b Desc="Total wing span" ToolLevel="1" Unit="m">34.10358666</b>
- <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.331683874</MAC>
- <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">122.4268024</S_ref>
- </ReferenceValues>
- <MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor>
- </Aerodynamics>
- <StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit">
- <Stabiliser>
- <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.03545133</VolumeCoefficient>
- <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.46074351</S_ref>
- </Stabiliser>
- <VerticalTail>
- <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.1018345125</VolumeCoefficient>
- <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">26.57458461</S_ref>
- </VerticalTail>
- </StabilityAndControlCharacteristics>
- <Performance Desc="Flugleistungen">
- <Range Desc="Reichweiten">
- <Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3043.938845</Range_maxPayloadatMTOM>
- <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">11558.21333</Range_maxFuelatMTOM>
- <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">3895.43595</Payload_maxFuelatMTOM>
- <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">12572.68487</Range_maxFuelEmpty>
- </Range>
- <Speed Desc="Fluggeschwindigkeiten">
- <M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise>
- <M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating>
- <V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating>
- <M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive>
- <V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive>
- <V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">161.952013</V_s1g>
- </Speed>
- <Altitudes Desc="Flughoehen">
- <h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise>
- <h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified>
- <h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">12010.7005</h_maxOperating>
- <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">12053.19642</h_maxCeiling>
- <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">7730.61576</h_maxOEI>
- </Altitudes>
- <Climb Desc="Steigflug">
- <TTC_Design Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">14.56137643</TTC_Design>
- <Time_to_1500ft_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10>
- <Time_to_ICA_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">15.53402313</Time_to_ICA_ISA10>
- <Range_to_ICA_ISA10 Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="NM">89.09881839</Range_to_ICA_ISA10>
- <Fuel_to_ICA_ISA10 Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="kg">1577.91233</Fuel_to_ICA_ISA10>
- <TTC_ISA Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA>
- <Time_to_1500ft_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA>
- <Time_to_ICA_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA>
- <Range_to_ICA_ISA Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA>
- <Fuel_to_ICA_ISA Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA>
- <TTC_ISA10_optROC Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA10_optROC>
- <Time_to_1500ft_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10_optROC>
- <Time_to_ICA_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA10_optROC>
- <Range_to_ICA_ISA10_optROC Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA10_optROC>
- <Fuel_to_ICA_ISA10_optROC Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA10_optROC>
- </Climb>
- <TakeOff Desc="Start Performance">
- <TakeOffDistance_Normal Desc="Startstrecke - Normalstartstrecke bei MTOM und ISA+15" ToolLevel="2" Unit="m">1731.705965</TakeOffDistance_Normal>
- <BFL Desc="Startstrecke - Balanced Fieldlength bei MTOM und ISA+15 " ToolLevel="2" Unit="m">1853.411621</BFL>
- <TimeToScreenHeight Desc="Zeit bis zum erreichen von 35 ft" ToolLevel="2" Unit="s">34.72221827</TimeToScreenHeight>
- <V_LOF Desc="Abhebegeschwindigkeit" ToolLevel="2" Unit="KCAS">136.8991062</V_LOF>
- <V_1 Desc="Decision Speed bei fuer MTOM BLFL" ToolLevel="2" Unit="KCAS">135.3462489</V_1>
- <V_2 Desc="Geschwindigkeit auf Screen height (35 ft)" ToolLevel="2" Unit="KCAS">136.8991062</V_2>
- <V_FTO Desc="Geschwindigkeit am Ende des Final T-O Segment (1500 ft)" ToolLevel="2" Unit="KCAS">203.0413711</V_FTO>
- <ScdSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.68313876</ScdSegmentClimbGradient>
- <FinalSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.683126144</FinalSegmentClimbGradient>
- </TakeOff>
- <Landing>
- <LandingDistance Desc="Landestrecke" ToolLevel="2" Unit="m">1528.071526</LandingDistance>
- <V_Approach Desc="Anfluggeschwindigkeit" ToolLevel="2" Unit="KCAS">129.2323788</V_Approach>
- </Landing>
- <MissionAnalysis Desc="Missionsanalyse">
- <DesignMission Desc="Parameter der Design-Mission">
- <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionDesign.xml</MissionFile>
- <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5008065466</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">18070.1076</Missionfuel>
- <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">14883.27019</Tripfuel>
- <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
- <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
- <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.947085161</Blocktime>
- <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.713751827</Flighttime>
- <Range Desc="Range" ToolLevel="3" Unit="NM">2500.55303</Range>
- <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">76962.57512</TOM>
- <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload>
- <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
- <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass>
- <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
- <Offtakes>
- <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
- <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">73.40008433</ShaftPowerTotal>
- <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
- </AverageCruiseOfftakes>
- </Offtakes>
- <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
- <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5148367758</CL_avg>
- <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4915188994</CL_min>
- <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5675400636</CL_max>
- </LiftCoefficientsCruise>
- <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
- <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">75060.13292</Mass_TOC>
- <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">62441.91279</Mass_TOD>
- </MassesCruise>
- </DesignMission>
- <StudyMission Desc="Parameter der Study-Mission">
- <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionStudy.xml</MissionFile>
- <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
- <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
- <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
- </CruiseStep>
- <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">5967.411758</Missionfuel>
- <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3241.768614</Tripfuel>
- <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
- <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
- <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.50538405</Blocktime>
- <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.272050716</Flighttime>
- <Range Desc="Range" ToolLevel="3" Unit="NM">500.546566</Range>
- <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">61467.87928</TOM>
- <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload>
- <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
- <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass>
- <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
- <Offtakes>
- <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
- <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">72.97412478</ShaftPowerTotal>
- <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
- </AverageCruiseOfftakes>
- </Offtakes>
- <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
- <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4681348875</CL_avg>
- <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4621586298</CL_min>
- <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4991350396</CL_max>
- </LiftCoefficientsCruise>
- <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
- <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">60071.12337</Mass_TOC>
- <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">58584.28057</Mass_TOD>
- </MassesCruise>
- </StudyMission>
- </MissionAnalysis>
- <RequirementsChecks>
- <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionReq.xml</MissionFile>
- <TLARs>
- <TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design>
- <LDN_Design Checked="1" ToolLevel="2">1</LDN_Design>
- <V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design>
- <h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design>
- <h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating>
- <h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI>
- <M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design>
- <TTC_Design Checked="1" ToolLevel="3">1</TTC_Design>
- </TLARs>
- <Certification>
- <climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment>
- <climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment>
- <climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI>
- <climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO>
- </Certification>
- </RequirementsChecks>
- </Performance>
- <MonetaryValues Desc="Kosten und Preise">
- <MonetaryScenario>
- <AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">12079799</AirframeEngineeringHours>
- <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">1500</ProductionVolume>
- </MonetaryScenario>
- <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">28158406</Earnings>
- <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">33855.557</NPV>
- <Prices Desc="Preise">
- <PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">71228241.8</PriceAirplane>
- <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0.07</DiscountRate>
- </Prices>
- <LCC Desc="Life Cycle Costs">
- <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
- <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">3475793421</NRCTotal>
- <NRCComponents>
- <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">1359777460</AirframeEngAndDesign>
- <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">345988343</DevSupportAndTesting>
- <FlightTestAC>
- <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">1636269510</FlightTestACTotal>
- <FlightTestACComponents>
- <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">117031730</EngineAndAvionics>
- <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">622590665</LaborManufacturing>
- <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">188900611</MaterialManufacturing>
- <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">624941946</Tooling>
- <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">82804558</QualityControl>
- </FlightTestACComponents>
- </FlightTestAC>
- <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">133758109</FlightTestOp>
- <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
- </NRCComponents>
- </NonRecurringCosts>
- <RecurringCosts Desc="Recurring Costs">
- <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">35766663</RCTotal>
- <RCComponents>
- <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">2408072</Wing>
- <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">2957731</Fuselage>
- <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">584113</Empennage>
- <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">639568</LandingGear>
- <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">879551</Pylons>
- <PowerUnit Desc="Costs for all installed engines with systems without pylons">
- <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">13337566</PowerUnitTotal>
- <PowerUnitComponents>
- <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">11357394</EquippedEngines>
- <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">1791842</Nacelles>
- <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">107416</BleedAirSystem>
- <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">80914</FuelSystem>
- </PowerUnitComponents>
- </PowerUnit>
- <Systems>
- <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">7436254</SystemsTotal>
- <SystemsComponents>
- <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">273442</APU>
- <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">220982</HydraulicSystem>
- <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">694499</AirConditioning>
- <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">40295</DeIcing>
- <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">39314</FireProtection>
- <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">598096</FlightControls>
- <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">343899</Instruments>
- <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">558835</AutomaticFlightSystem>
- <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">2278329</Navigation>
- <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">1117671</Communication>
- <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">1270893</ElectricalSystem>
- </SystemsComponents>
- </Systems>
- <Furnishings>
- <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">1442699</FurnishingsTotal>
- <FurnishingsComponents>
- <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">1048900</Furnishing>
- <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">41911</FixedEmergencyOxygen>
- <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">228444</Lighting>
- <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">123443</WaterInstallation>
- </FurnishingsComponents>
- </Furnishings>
- <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">1415894</OperatorsItems>
- <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">4665217</FinalAssembly>
- </RCComponents>
- </RecurringCosts>
- <OperatingCosts>
- <OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal">
- <FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">2230</FlightsPerYear>
- <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">1</SeatLoadFactor>
- </OperatingScenario>
- <DirectOperatingCosts>
- <DOC_total Desc="Summe aller DOCComponents (s.u)">
- <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">20437514.98</DOC_year>
- <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7204.76</DOC_FH>
- <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9164.81</DOC_flight>
- <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">9.9</DOC_km>
- <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.6</DOC_100ASK>
- </DOC_total>
- <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
- <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">17054173.5</COC_year>
- <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">6012.05</COC_FH>
- <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">7647.62</COC_flight>
- <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">8.26</COC_km>
- <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">5.50770807</COC_100ASK>
- </COC_total>
- <DOCComponents Desc="DOC-Anteile in 100ASK">
- <Charge Desc="Gebuehren pro 100ASK">
- <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">1.83</ChargeTotal>
- <ChargesComponents>
- <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0.73</NavigationCharge>
- <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0.33</LandingCharge>
- <LandingChargeComponents>
- <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge>
- <NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge>
- <ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0.33</ChargeWithoutEmission>
- </LandingChargeComponents>
- <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0.77</GroundCharge>
- </ChargesComponents>
- </Charge>
- <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0.98</Depreciation>
- <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0.11</Insurance>
- <Maintenance Desc="Wartungskosten">
- <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0.75</MaintenanceTotal>
- <MaintenanceComponents>
- <Airframe Desc="Wartungskosten Airframe">
- <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0.3</AirframeTotal>
- <CostComponents>
- <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.243</LabourCosts>
- <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.061</MaterialCosts>
- </CostComponents>
- <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
- <ATA21 Desc="Environmental Control System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0134</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0107</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0027</MaterialCosts>
- </CostComponents>
- </ATA21>
- <ATA22 Desc="Autoflight">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0127</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0102</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
- </CostComponents>
- </ATA22>
- <ATA23 Desc="Communications">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0123</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0098</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
- </CostComponents>
- </ATA23>
- <ATA24 Desc="Electrical System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0211</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0169</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0042</MaterialCosts>
- </CostComponents>
- </ATA24>
- <ATA25 Desc="Furnishing">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0409</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0327</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0082</MaterialCosts>
- </CostComponents>
- </ATA25>
- <ATA26 Desc="Fire Protection">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0043</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0035</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0009</MaterialCosts>
- </CostComponents>
- </ATA26>
- <ATA27 Desc="Flight Control System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.025</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.02</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.005</MaterialCosts>
- </CostComponents>
- </ATA27>
- <ATA28 Desc="Fuel System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0022</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
- </CostComponents>
- </ATA28>
- <ATA29 Desc="Hydraulic System">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0131</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0105</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0026</MaterialCosts>
- </CostComponents>
- </ATA29>
- <ATA30 Desc="Ice and Rain Protection">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
- </CostComponents>
- </ATA30>
- <ATA31 Desc="Instrumentation">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0013</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
- </CostComponents>
- </ATA31>
- <ATA32 Desc="Landing Gear">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0559</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0447</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0112</MaterialCosts>
- </CostComponents>
- </ATA32>
- <ATA33 Desc="Lights">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0051</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0041</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</MaterialCosts>
- </CostComponents>
- </ATA33>
- <ATA34 Desc="Navigation">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0142</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0113</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0028</MaterialCosts>
- </CostComponents>
- </ATA34>
- <ATA35 Desc="Oxygen">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.003</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0006</MaterialCosts>
- </CostComponents>
- </ATA35>
- <ATA36 Desc="Pneumatic">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0036</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0029</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0007</MaterialCosts>
- </CostComponents>
- </ATA36>
- <ATA38 Desc="Water and Waste">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0019</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0005</MaterialCosts>
- </CostComponents>
- </ATA38>
- <ATA49 Desc="APU">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0104</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0083</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0021</MaterialCosts>
- </CostComponents>
- </ATA49>
- <ATA51 Desc="Structure">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.004</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0032</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0008</MaterialCosts>
- </CostComponents>
- </ATA51>
- <ATA52 Desc="Doors">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0054</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0044</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA52>
- <ATA53 Desc="Fuselage">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0057</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA53>
- <ATA54 Desc="Nacelles">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0002</MaterialCosts>
- </CostComponents>
- </ATA54>
- <ATA55 Desc="Stabilizers">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
- </CostComponents>
- </ATA55>
- <ATA56 Desc="Windows">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0081</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0065</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</MaterialCosts>
- </CostComponents>
- </ATA56>
- <ATA57 Desc="Wings">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0056</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
- </CostComponents>
- </ATA57>
- <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
- <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0294</TotalCosts>
- <CostComponents>
- <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0235</LabourCosts>
- <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0059</MaterialCosts>
- </CostComponents>
- </ATA99>
- </AirframeComponents>
- </Airframe>
- <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0.45</Engine>
- </MaintenanceComponents>
- </Maintenance>
- <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">2.44</Fuel>
- <Crew Desc="Crew Kosten">
- <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0.49</CrewTotal>
- <CrewComponents>
- <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.12</FlightCrew>
- <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.36</CabinCrew>
- </CrewComponents>
- </Crew>
- <Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay>
- </DOCComponents>
- </DirectOperatingCosts>
- <IndirectOperatingCosts>
- <IOC_total Desc="Summe aller IOCComponents (s.u)">
- <IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">20699680.51</IOC_year>
- <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7297.17</IOC_FH>
- <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9282.37</IOC_flight>
- <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">10.02</IOC_km>
- <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.68</IOC_100ASK>
- </IOC_total>
- </IndirectOperatingCosts>
- </OperatingCosts>
- <EndOfLifeCosts>
- <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">48616</EOLCTotal>
- <EOLCTotalComponents>
- <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">9140</TransportToEoLSite>
- <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">124837</DisassemblyAndDismantling>
- <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">-86485</Recycling>
- <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">297</Incineration>
- <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">827</Landfill>
- </EOLCTotalComponents>
- </EndOfLifeCosts>
- </LCC>
- </MonetaryValues>
- <EcologicalValues Desc="Oekologische Bewertung">
- <Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse">
- <NoisePathFiles>
- <Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure>
- <Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach>
- </NoisePathFiles>
- <NoiseCertificationLevels>
- <LateralPoint>
- <LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower>
- <SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </LateralPoint>
- <FlyoverPoint>
- <Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover>
- <SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </FlyoverPoint>
- <ApproachPoint>
- <Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach>
- <SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </ApproachPoint>
- <CumulativeValues>
- <EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB>
- <SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </CumulativeValues>
- </NoiseCertificationLevels>
- <CommunityNoiseLevels>
- <TakeOff>
- <SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL>
- <SPLarea>
- <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
- <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
- </SPLarea>
- <PNLarea>
- <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
- <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
- </PNLarea>
- <PNLTarea>
- <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
- <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
- </PNLTarea>
- <EPNLarea>
- <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
- <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
- </EPNLarea>
- <LoudnessArea>
- <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
- <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
- </LoudnessArea>
- <TonalityArea>
- <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
- <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
- <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
- <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
- </TonalityArea>
- <SharpnessArea>
- <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
- <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
- </SharpnessArea>
- <PsychoacousticAnnoyanceArea>
- <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
- <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
- </PsychoacousticAnnoyanceArea>
- <SELarea Desc="Sound Exposure Level area">
- <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
- <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
- <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
- <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
- </SELarea>
- </TakeOff>
- <Approach>
- <SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL>
- <SPLarea>
- <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
- <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
- </SPLarea>
- <PNLarea>
- <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
- <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
- </PNLarea>
- <PNLTarea>
- <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
- <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
- </PNLTarea>
- <EPNLarea>
- <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
- <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
- </EPNLarea>
- <LoudnessArea>
- <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
- <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
- </LoudnessArea>
- <TonalityArea>
- <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
- <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
- <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
- <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
- </TonalityArea>
- <SharpnessArea>
- <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
- <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
- </SharpnessArea>
- <PsychoacousticAnnoyanceArea>
- <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
- <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
- </PsychoacousticAnnoyanceArea>
- <SELarea Desc="Sound Exposure Level area">
- <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
- <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
- <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
- <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
- </SELarea>
- </Approach>
- <CumulativeValues>
- <EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB>
- <SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL>
- <Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness>
- <Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
- <Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness>
- <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
- </CumulativeValues>
- </CommunityNoiseLevels>
- </Noise>
- <Emissions>
- <Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm">
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">11763648.53</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">40697548.71</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">22681.579</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">506.978</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">10059.553</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">16890.095</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">176.255</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">982.444</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0.019</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">1432.078</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-4663.364</HC>
- </Development>
- <Production>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">618228.677</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">5361791.97</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">1320.026</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">1715.593</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">2280.541</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">1327.591</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">5.711</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-5.298</HC>
- </Production>
- <Operations>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">649479288.1</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">269362047.2</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">821056.648</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">279870.45</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">533623.487</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">749253.374</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">10631.577</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-247022.508</HC>
- <OperationComponents>
- <ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">2844.948</CO2>
- <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">1084.134</H2O>
- <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.759</SO2>
- <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">99.106</HC>
- <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">5.747</CO>
- <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">11.071</NOx>
- <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.023</PM10>
- </ICAO_LTO>
- <Mission Desc="Environmental analysis of one study mission">
- <LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)">
- <Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">19.622</Total>
- <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">14</TaxiTime>
- <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0.311</TakeOffTime>
- <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0.933</ClimbOutTime>
- <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">4.377</ApproachTime>
- </LTOTimes>
- <LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">1500.242</CO2>
- <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">571.702</H2O>
- <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.4</SO2>
- <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">-2.376</HC>
- <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">2.018</CO>
- <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">3.831</NOx>
- <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.009</PM10>
- </LTO>
- <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
- <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">9149.073</CO2>
- <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">3486.468</H2O>
- <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">2.441</SO2>
- <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">-2.055</HC>
- <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">1.349</CO>
- <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">7.688</NOx>
- <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0.01</PM10>
- </Cruise>
- </Mission>
- </OperationComponents>
- </Operations>
- <EndOfLife>
- <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">-114694.14</CO2>
- <H2O Desc="Wasser" ToolLevel="1" Unit="kg">-1466106.754</H2O>
- <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">-495.854</NOx>
- <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">-1949.608</CO>
- <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">-1061.466</SO2>
- <CH4 Desc="Methan" ToolLevel="1" Unit="kg">-304.18</CH4>
- <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0.419</PM10>
- <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
- <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
- <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
- <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-3.735</HC>
- </EndOfLife>
- </Emissions>
- <CED Desc="Cumulative Energy Demand">
- <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">1.033604491e+16</CEDTotal>
- <CEDComponents>
- <Development Desc="Development" ToolLevel="1" Unit="MJ">2.115958924e+14</Development>
- <Production Desc="Production" ToolLevel="1" Unit="MJ">1.332765215e+13</Production>
- <Operations Desc="Operation" ToolLevel="1" Unit="MJ">1.011292433e+16</Operations>
- <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">-1.802957726e+12</EndOfLife>
- </CEDComponents>
- </CED>
- <ClimateImpact Desc="Climate Impact due to Aircraft Operation">
- <ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0.0014420111</ATR>
- <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">2.13271e-05</AGTP>
- <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">3.52252e-05</AGTP100>
- <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">4.29914e-05</AGWP>
- <AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100>
- </ClimateImpact>
- <AirQuality Desc="Climate Impact due to Aircraft Operation">
- <ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-">
- <HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">-0.4355</HC>
- <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0.0614</CO>
- <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0.1915</NOx>
- <soot Desc="TF Russ" ToolLevel="1" Unit="-">0.0767</soot>
- </ToleranceFactors>
- <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">-0.0265</AirQualityIndex>
- </AirQuality>
- </EcologicalValues>
- <Requirements Desc="Designforderungen">
- <m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload>
- <m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload>
- <DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
- <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
- <TOFL_Design Desc="Auslegungsstartstrecke (Balanced Field Length)" Unit="m">2200</TOFL_Design>
- <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+10)" Unit="min">35</TTC_Design>
- <ClimbGradients Desc="Steiggradientenforderungen">
- <secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment>
- <finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment>
- <approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO>
- <approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI>
- </ClimbGradients>
- <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
- <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
- </ClimbSpeedSchedule>
- <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- </DescentSpeedSchedule>
- <h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design>
- <M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design>
- <LDN_Design Desc="Auslegungslandestrecke (Sicherheitslandestrecke)" Unit="m">1850</LDN_Design>
- <V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design>
- <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
- <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
- <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
- <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
- <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
- </DesignMission>
- <StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
- <R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design>
- <m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload>
- <NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX>
- <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
- <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
- </ClimbSpeedSchedule>
- <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
- <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
- <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
- </DescentSpeedSchedule>
- <h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise>
- <M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise>
- <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
- <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
- <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
- <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
- <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
- </StudyMission>
- <FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod>
- <V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed>
- <DesignFlightEnvelope>
- <VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO>
- <MMO Desc="Max operating Mach No." Unit="-">0.82</MMO>
- <h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating>
- <h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI>
- </DesignFlightEnvelope>
- <SizeLimits Desc="maximale geometrische Abmasse">
- <SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit>
- </SizeLimits>
- <ACN Desc="Aircraft Classification Number">
- <ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType>
- <ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory>
- <ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit>
- </ACN>
- </Requirements>
- <DesignSpecification Desc="Spezifikation des Entwurfs">
- <Configuration Desc="Qualitative Beschreibung der Konfiguration">
- <Wing Desc="Parameter des Fluegels">
- <Position Desc="Fluegellage low, mid, high" Unit="-">low</Position>
- </Wing>
- <Stabiliser Desc="Parameter des Hoehenleitwerks">
- <h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing>
- </Stabiliser>
- <LandingGear Desc="Fahrwerksanordnung">
- <MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition>
- <Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable>
- </LandingGear>
- <Fuselage Desc="Fuselage parameters">
- <Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized>
- </Fuselage>
- <CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType>
- <Fin Desc="Parameter des Seitenleitwerks">
- <FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig>
- </Fin>
- </Configuration>
- <Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen">
- <MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX>
- <PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks>
- <PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1">
- <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes>
- <Class Desc="Definition der Klasse" ID="1">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats>
- </Class>
- <Class Desc="Definition der Klasse" ID="2">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">33</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats>
- </Class>
- <Class Desc="Definition der Klasse" ID="3">
- <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType>
- <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
- <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats>
- </Class>
- </PAXDeck>
- </Accommodation>
- <Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs">
- <CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks>
- <CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1">
- <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments>
- <Compartment Desc="Definition des Compartments" ID="1">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs>
- </ULDType>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="2">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs>
- </ULDType>
- </Compartment>
- <Compartment Desc="Definition des Compartments" ID="3">
- <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType>
- <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
- <ULDType Desc="Definition der Containergruppe" ID="1">
- <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
- <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
- <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs>
- </ULDType>
- </Compartment>
- </CargoDeck>
- </Cargo>
- <Propulsion Desc="Vorgaben zum Antriebssystem">
- <TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine>
- <NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines>
- <PositionOfEngines Desc="Positionierung der Triebwerke">
- <EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing>
- <EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage>
- <EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage>
- <WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition>
- </PositionOfEngines>
- <FuelDensity Desc="Dichte des Kraftstoffs" Unit="kg/l">0.785</FuelDensity>
- </Propulsion>
- <TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks">
- <NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks>
- <NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks>
- <NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks>
- </TankConfiguration>
- <HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem">
- <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.3</C_LmaxT-O>
- <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding>
- </HighLiftSystem>
- <DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen">
- <n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1>
- <n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2>
- </DesignLoads>
- <Technology Desc="Vorgaben spezieller Technologien">
- <LaminarFlow Desc="HLFC oder NLF">
- <Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird">
- <Wing>
- <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
- <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
- </Wing>
- <Stabilizer>
- <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
- <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
- </Stabilizer>
- <Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin>
- <Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles>
- </Components>
- </LaminarFlow>
- <ElectricTaxiing>
- <DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing>
- <EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime>
- </ElectricTaxiing>
- <BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem>
- </Technology>
- </DesignSpecification>
-</AcftExchangeFile>