From 6f7b33c9665d38c32f62763ee6872c203277cdc6 Mon Sep 17 00:00:00 2001
From: Sebastian Oberschwendtner <sebastian.oberschwendtner@tum.de>
Date: Tue, 19 Sep 2023 14:33:52 +0200
Subject: [PATCH] Adds first version for documenting the AcXML.
---
.gitignore | 5 +-
README.md | 24 +
mkdocs.yml | 15 +
scripts/CSR-02.xml | 3767 ++++++++++++++++++++++++++++++
scripts/document_aircraft_xml.py | 233 ++
5 files changed, 4043 insertions(+), 1 deletion(-)
create mode 100644 scripts/CSR-02.xml
create mode 100644 scripts/document_aircraft_xml.py
diff --git a/.gitignore b/.gitignore
index 3828992..d9dd1e0 100644
--- a/.gitignore
+++ b/.gitignore
@@ -1,2 +1,5 @@
# Ignore generated Doxygen docs in modules folder
-/docs/modules/**/
+docs/modules/**/
+
+# Ignore the local docs of the AcXML
+docs/aircraft-xml/
diff --git a/README.md b/README.md
index d3168f8..6e94ace 100644
--- a/README.md
+++ b/README.md
@@ -39,4 +39,28 @@ date: yyyy-mm-dd
# MyPage
<Content goes here>
+```
+
+# Tools
+The documentation page uses some custom tools to enable a seamless continuous documentation:
+
+## document_aircraft_xml.py
+> Script
+
+This script is used to document the aircraft exchange file.
+It parses the XML file and creates the documentation for each node using its description.
+
+The usage is explained in the output when calling the script with the `--help` option:
+```sh
+usage: document_aircraft_xml.py [-h] [--title title] [--level level] filename
+
+Converts an aircraft XML file to a markdown file. The output is streamed to stdout and can be piped to a file.
+
+positional arguments:
+ filename The XML file to convert.
+
+options:
+ -h, --help show this help message and exit
+ --title title The title of the output page. This also sets the root node which is used to create the document.
+ --level level The maximum level nodes to be used as headers.
```
\ No newline at end of file
diff --git a/mkdocs.yml b/mkdocs.yml
index 66f4f38..61c66f9 100644
--- a/mkdocs.yml
+++ b/mkdocs.yml
@@ -104,6 +104,21 @@ nav:
- 'Style Guide':
- 'C++': 'developer/style/cpp.md'
- 'Python': 'developer/style/python.md'
+ - 'Aircraft Exchange File':
+ - 'General': 'aircraft-xml/general.md'
+ - 'MassesAndLoadings': 'aircraft-xml/masses.md'
+ - 'Geometry': 'aircraft-xml/geometry.md'
+ - 'Structure': 'aircraft-xml/structure.md'
+ - 'Accommodation': 'aircraft-xml/accommodation.md'
+ - 'Propulsion': 'aircraft-xml/propulsion.md'
+ - 'Systems': 'aircraft-xml/systems.md'
+ - 'Aerodynamics': 'aircraft-xml/aerodynamics.md'
+ - 'StabilityAndControlCharacteristics': 'aircraft-xml/stability.md'
+ - 'Performance': 'aircraft-xml/performance.md'
+ - 'MonetaryValues': 'aircraft-xml/monetary.md'
+ - 'EcologicalValues': 'aircraft-xml/ecological.md'
+ - 'Requirements': 'aircraft-xml/requirements.md'
+ - 'DesignSpecification': 'aircraft-xml/specification.md'
- 'About':
- 'license.md'
- 'contact.md'
diff --git a/scripts/CSR-02.xml b/scripts/CSR-02.xml
new file mode 100644
index 0000000..e79520e
--- /dev/null
+++ b/scripts/CSR-02.xml
@@ -0,0 +1,3767 @@
+<AcftExchangeFile>
+ <General Desc="Allgemeine Angaben">
+ <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
+ <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-02</Model>
+ </General>
+ <MassesAndLoadings Desc="-">
+ <MassBreakdown Desc="Mass breakdown">
+ <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
+ <Mass ToolLevel="1" Unit="kg">8288.967026</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">17.1682343</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">-1.030900284</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">6063.492374</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">17.1682343</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">-1.030900284</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">2225.474652</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
+ <Mass ToolLevel="1" Unit="kg">282.297482</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ </FixedLeadingEdge>
+ <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
+ <Mass ToolLevel="1" Unit="kg">380.8095925</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ </MovableLeadingEdge>
+ <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
+ <Mass ToolLevel="1" Unit="kg">546.1954554</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ </FixedTrailingEdge>
+ <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
+ <Mass ToolLevel="1" Unit="kg">1016.172122</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">17.1682343</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">-1.030900284</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ </Miscellaneous>
+ </Wing>
+ <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">8482.604033</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">16.88739053</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">1325.468005</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">33.95934635</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">1.654512598</h_Item>
+ </RefPoint>
+ <Tailplane Desc="Airbus Chapter 13">
+ <Mass ToolLevel="1" Unit="kg">759.3554913</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">34.25726239</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">1.654512598</h_Item>
+ </RefPoint>
+ </Tailplane>
+ <Fin Desc="Airbus Chapter 14">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">566.1125139</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">33.55973642</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">1.654512598</h_Item>
+ </RefPoint>
+ </Fin>
+ </Empennage>
+ <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2600.672138</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">15.45985449</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">-1.413319125</h_Item>
+ </RefPoint>
+ <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">390.1008207</Mass>
+ <RefPoint Desc="Position of NoseGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">1.947356458</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">-1.978883883</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">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
+ <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</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">-1.313513579</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">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
+ <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</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">-1.313513579</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">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
+ <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">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
+ <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">1302.156306</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">15.87054623</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">-1.53285849</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">8513.660953</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">14.78507499</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">-2.958381704</h_Item>
+ </RefPoint>
+ <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">4009.674109</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</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">4009.674109</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</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">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</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">172.6795332</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">16.05413654</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">-1.27103384</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">321.6332021</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">17.1682343</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">-1.030900284</h_Item>
+ </RefPoint>
+ </FuelSystem>
+ </PowerUnit>
+ <Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
+ <Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5355.445849</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">16.39637449</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">-0.5741904671</h_Item>
+ </RefPoint>
+ <APU Desc="Airbus Chapter 30, ATA49">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">254.7995941</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">35.65115779</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">184.4172612</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">16.05413654</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">-1.27103384</h_Item>
+ </RefPoint>
+ </HydraulicGeneration>
+ <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">805.6612438</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">16.05413654</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">-1.27103384</h_Item>
+ </RefPoint>
+ </HydraulicDistribution>
+ <AirConditioning Desc="Airbus Chapter 33, ATA21">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">717.7462397</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">16.05413654</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">-1.27103384</h_Item>
+ </RefPoint>
+ </AirConditioning>
+ <DeIcing Desc="Airbus Chapter 34, ATA30">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">42.30906964</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">16.88739053</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">94.97439103</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">16.88739053</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">711.5018356</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">16.05413654</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">-1.27103384</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">43.35817647</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">94.98684287</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">33.35895545</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">64.77541722</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">147.1812978</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">39.74320013</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">145.7975785</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">142.3003671</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">85.52867064</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">4.125269051</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">138.9840898</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">12.51238234</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">566.627443</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">12.51238234</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">277.9681796</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">12.51238234</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">779.0134574</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">16.88739053</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">695.9143735</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">16.88739053</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">3108.708964</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">16.88739053</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">2452.022285</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">16.88739053</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">16.88739053</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">268.2126788</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">16.88739053</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">16.88739053</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">3331.623637</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">14.6792334</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">1581.073637</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">16.71467966</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">12.84084522</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">66724.81066</MLM>
+ <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">79148.59668</MTOM>
+ <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
+ <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38977.68327</MME>
+ <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">42309.30691</OME>
+ <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">62309.30691</MZFM>
+ <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
+ <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">32478.96446</MaximumUsableFuel>
+ <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">625.8366729</WingLoading>
+ <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3320609465</ThrustToWeight>
+ <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
+ <MassMomentsOfInertia Desc="Mass moment of inertia (MMoI)">
+ <DesignPoint Desc="MMoI at Designpoint">
+ <Jxx Desc="MMoI x-axis" ToolLevel="1" Unit="kg*m2">1200828.866</Jxx>
+ <Jyy Desc="MMoI y-axis" ToolLevel="1" Unit="kg*m2">3139142.531</Jyy>
+ <Jzz Desc="MMoI z-axis" ToolLevel="1" Unit="kg*m2">4166372.541</Jzz>
+ <Jxy Desc="MMoI xy-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxy>
+ <Jxz Desc="MMoI xz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxz>
+ <Jyz Desc="MMoI yz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jyz>
+ </DesignPoint>
+ </MassMomentsOfInertia>
+ <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">-0.7482016769</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.80339635</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">-0.9750336151</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.67440503</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">-0.9992954046</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.88886532</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">12.51238234</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">-1.27103384</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">geometryData\airfoilData\F15_15.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_12.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">7.083508401</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.434391811</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.199184069</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">geometryData\airfoilData\F15_12.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_11.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.434391811</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.053794453</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">12.1314295</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="-">0.1168298891</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="-">0.2054149445</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="-">0.1168298891</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">31.6591417</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">1.654512598</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">-1.250900566</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.992016088</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.123933623</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.439701701</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">29.86369528</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">1.654512598</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.787462516</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.531274612</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.952800274</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">-0.5232505048</h_Tip>
+ </TipSegment>
+ <NoseSegment ID="1">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6219072875</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.647944796</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06445732892</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5232505048</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="2">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.232171749</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.283759313</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.1933719868</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4278783272</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="3">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.81877794</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.894925056</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3222866446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3362034659</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="4">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.368913086</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.468092813</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4512013025</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2502283023</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="5">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.868421677</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.988514422</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.5801159603</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1721650609</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="6">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.301028172</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.439232935</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7090306182</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1045572839</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="7">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.6471193</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.799813925</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.837945276</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05047013554</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="8">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.881644273</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.044157799</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.9668599339</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01381855438</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="9">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.095774592</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">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">16.76076782</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">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.074891643</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.03069492579</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="2">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.889781167</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.1232501637</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="3">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.892703799</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.578053688</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.2791139033</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="4">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.618301624</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.143415874</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.4964328104</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="5">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.142809701</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.681089784</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.7275958556</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="6">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.985033</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.754173041</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.191054227</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="7">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.654512598</deltah_Segment>
+ </TailSegment>
+ </TailDescription>
+ </FuselageParameters>
+ </Fuselage>
+ <Nacelle Desc="Beschreibung der inneren rechten Triebwerksgondel" ID="InnerRightWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">5.49297931</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</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">20</Points>
+ <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="3">
+ <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="4">
+ <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">geometryData\nacelle.dat</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</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 inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-5.49297931</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</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">20</Points>
+ <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="3">
+ <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="4">
+ <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">geometryData\nacelle.dat</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</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 aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle">
+ <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 aeusseren linken Triebwerksgondel" ID="OuterLeftWingNacelle">
+ <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 rechten Hecktriebwerksgondel" ID="RightFuselageNacelle">
+ <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 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">13.57788621</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.49297931</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</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">71.83066751</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">13.57788621</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.49297931</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</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">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</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">71.83066751</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">3.480695762</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">-1.978883883</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">3.480695762</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">-5.04556249</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">17.84441297</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</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">17.80664751</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</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">17.84441297</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</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">17.80664751</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</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">2</NoOfSeatTypes>
+ <seat Desc="Description of seat" ID="1">
+ <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="2">
+ <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>
+ <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">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</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</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>
+ </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">186.1462316</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">97.50130651</A_CabinDeck>
+ <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
+ <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.63012573</w_CabinDeck>
+ <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.85893376</l_CabinDeck>
+ <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">184.2960557</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">5.983021821</x_center>
+ </Class>
+ <Class Desc="Definition der Klasse" ID="2">
+ <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.4124887</x_center>
+ </Class>
+ </CabinDeck>
+ </Cabin>
+ <Cargo Desc="Beschreibung des Frachtraums">
+ <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">35.92426606</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">56.63668783</A_CargoDeck>
+ <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
+ <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.280233538</w_CargoDeck>
+ <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">17.26605352</l_CargoDeck>
+ <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">36.40649695</V_CargoDeck>
+ <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.7695477</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">4.84</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">6.37</Length>
+ <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">18.82863715</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="-">1.168175939</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="-">engineData\V2527-A5\V2527-A5.xml</EngineDataFile>
+ <JetEngineData Desc="Jet spezifische Triebwerksdaten">
+ <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">128.8646365</SeaLevelStaticThrust>
+ <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.743365695</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">1.976823221</w_Engine>
+ <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.289180745</h_Engine>
+ <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.710701279</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+deltaISA(Requirements/DesignMission), SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">127.3858501</EquivalentThrust>
+ <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">128.8646365</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.316357232</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01021503857</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9783203125</N1>
+ </MaximumTakeOff>
+ <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">101.9086801</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.329201509</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01304306471</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9734765625</N1>
+ </MaximumGoAround>
+ <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+deltaISA(Requirements/DesignMission) bei" Mach="0.8">
+ <MaxThrust Desc="Without Offtakes">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">32.18450048</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5460196217</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01696529738</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.981796875</N1>
+ </MaxThrust>
+ <BucketThrust Desc="Without Offtakes">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4959848906</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01693808075</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</N1>
+ </BucketThrust>
+ <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5130623087</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01752128136</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</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="Centre tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">10541.14749</TankVolume>
+ </CentreTank>
+ <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
+ <WingTank Desc="Wing tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
+ </WingTank>
+ <WingTank Desc="Wing tank description" ID="2">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
+ </WingTank>
+ <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
+ <TrimTank Desc="Trim tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
+ </TrimTank>
+ <FuselageTanks Desc="No of fuselage tanks" ToolLevel="1">0</FuselageTanks>
+ <FuselageTank Desc="Fuselage tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
+ </FuselageTank>
+ <TotalFuelVolume Desc="Total fuel volume of all tanks" ToolLevel="1" Unit="l">41374.47702</TotalFuelVolume>
+ </FuelTank>
+ <ATA21_EnvironmentalControlSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.37098678</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">1.31382376</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">93.56406668</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">12.23167268</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">7.451202472</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">0.6613272863</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">74.97503685</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">7.884251516</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">0.1039553182</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">-205.4781816</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-181.0078664</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.188533015</BleedAir>
+ </DesignPower>
+ </ATA70_PropulsionSystem>
+ </Systems>
+ <Aerodynamics Desc="Aerodynamik">
+ <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">16.46037111</LoverD_Cruise>
+ <LiftCoefficients Desc="Auftriebsbeiwerte">
+ <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5381848981</C_L_design>
+ <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.916185004</C_LmaxLanding>
+ <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.515329503</C_LmaxT-O>
+ <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.528</C_LoptimumCruise>
+ <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.5626638406</C_L_opt_wing>
+ <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03466354382</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="-">0.03207704106</C_D_total>
+ <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.009803808575</C_D_ind>
+ <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
+ <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01972511904</C_D_visc_total>
+ <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00660550988</C_D_visc_wing>
+ <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001454379701</C_D_visc_stab>
+ <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001569261547</C_D_visc_fin>
+ <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006412233533</C_D_visc_fus>
+ <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001743616971</C_D_visc_nac>
+ <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.001940117406</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="-">0.002548113448</C_D_wave_total>
+ <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.002547491352</C_D_wave_wing>
+ <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">6.220952302e-07</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="-">1.138318599e-05</C_M_total>
+ </MomentCoefficients>
+ <Polar Desc="Flugzeugpolare">
+ <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">aeroData\CSR-02_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">34.66122714</b>
+ <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.402512853</MAC>
+ <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">126.463228</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="-">1.017690098</VolumeCoefficient>
+ <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.94519006</S_ref>
+ </Stabiliser>
+ <VerticalTail>
+ <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.09489408521</VolumeCoefficient>
+ <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">25.44285876</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">3246.670783</Range_maxPayloadatMTOM>
+ <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">10458.2771</Range_maxFuelatMTOM>
+ <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">4360.32531</Payload_maxFuelatMTOM>
+ <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">10709.69495</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">154.8031322</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">11713.23959</h_maxOperating>
+ <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">11763.23474</h_maxCeiling>
+ <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">6608.028951</h_maxOEI>
+ </Altitudes>
+ <Climb Desc="Climb Performance">
+ <TTC_Design Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_Design>
+ <TTC_ISA Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_ISA>
+ <Time_to_1500ft_ISA Desc="Time needed to climb from BR to 1500ft (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">1.251683745</Time_to_1500ft_ISA>
+ <Time_to_ICA_ISA Desc="Time needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">17.41051663</Time_to_ICA_ISA>
+ <Range_to_ICA_ISA Desc="Range needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="NM">101.9061674</Range_to_ICA_ISA>
+ <Fuel_to_ICA_ISA Desc="Fuel mass needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="kg">1715.660845</Fuel_to_ICA_ISA>
+ </Climb>
+ <TakeOff Desc="Start Performance">
+ <TakeOffDistance_Normal Desc="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">660.3942437</TakeOffDistance_Normal>
+ <TakeOffDistance_Normal_Safety Desc="Takeoff distance at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission) (incl. 15 percent safety margin; estimated by calculatePerformance)" ToolLevel="2" Unit="m">1314.175463</TakeOffDistance_Normal_Safety>
+ <BFL Desc="Design takeoff distance - Balanced Field Length at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="m">0</BFL>
+ <TimeToScreenHeight Desc="Time until reaching screen height (35ft) at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="s">28.99214318</TimeToScreenHeight>
+ <V_LOF Desc="Lift-off speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">126.3711884</V_LOF>
+ <V_1 Desc="Decision Speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">0</V_1>
+ <V_2 Desc="Speed at screen height (35 ft)" ToolLevel="2" Unit="KCAS">126.3711884</V_2>
+ <V_FTO Desc="Speed at final takeoff segment (1500 ft)" ToolLevel="2" Unit="KCAS">202.4392823</V_FTO>
+ <ScdSegmentClimbGradient Desc="Climb gradient in second takeoff segment" ToolLevel="2" Unit="%">2.416614712</ScdSegmentClimbGradient>
+ <FinalSegmentClimbGradient Desc="Climb gradient in final takeoff segment" ToolLevel="2" Unit="%">2.416614712</FinalSegmentClimbGradient>
+ </TakeOff>
+ <Landing>
+ <LandingDistance Desc="Landing distance at Sea Level for MLM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">1373.253939</LandingDistance>
+ <NeededRunwayLength Desc="Needed runway length at Sea Level with MLM and ISA+deltaISA(Requirements/DesignMission)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" ToolLevel="2" Unit="m">1680.105692</NeededRunwayLength>
+ <V_Approach Desc="Final Approach Speed" ToolLevel="2" Unit="KCAS">128.6850003</V_Approach>
+ </Landing>
+ <MissionAnalysis Desc="Missionsanalyse">
+ <DesignMission Desc="Parameter der Design-Mission">
+ <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\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="-">0.5009643041</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">19940.80556</Missionfuel>
+ <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">16588.93118</Tripfuel>
+ <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5157969</TaxifuelTakeoff>
+ <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39766495</TaxifuelLdg>
+ <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.94079849</Blocktime>
+ <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.707465156</Flighttime>
+ <Range Desc="Range" ToolLevel="3" Unit="NM">2500.496213</Range>
+ <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">79148.59668</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">103.3245182</ShaftPowerTotal>
+ <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
+ </AverageCruiseOfftakes>
+ </Offtakes>
+ <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+ <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5101767772</CL_avg>
+ <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4831782814</CL_min>
+ <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5667676169</CL_max>
+ </LiftCoefficientsCruise>
+ <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+ <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">77451.03811</Mass_TOC>
+ <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">63267.90838</Mass_TOD>
+ </MassesCruise>
+ </DesignMission>
+ <StudyMission Desc="Parameter der Study-Mission">
+ <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\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">6746.530829</Missionfuel>
+ <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3818.187572</Tripfuel>
+ <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5158315</TaxifuelTakeoff>
+ <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39768417</TaxifuelLdg>
+ <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.499139745</Blocktime>
+ <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.265806411</Flighttime>
+ <Range Desc="Range" ToolLevel="3" Unit="NM">500.6435758</Range>
+ <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">62562.32191</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">102.8677337</ShaftPowerTotal>
+ <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
+ </AverageCruiseOfftakes>
+ </Offtakes>
+ <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+ <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4609914236</CL_avg>
+ <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4538594196</CL_min>
+ <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4925634903</CL_max>
+ </LiftCoefficientsCruise>
+ <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+ <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">61280.43659</Mass_TOC>
+ <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">59428.93455</Mass_TOD>
+ </MassesCruise>
+ </StudyMission>
+ </MissionAnalysis>
+ <RequirementsChecks>
+ <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionData\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">0</AirframeEngineeringHours>
+ <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">0</ProductionVolume>
+ </MonetaryScenario>
+ <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">0</Earnings>
+ <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">0</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="$">0</PriceAirplane>
+ <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0</DiscountRate>
+ </Prices>
+ <LCC Desc="Life Cycle Costs">
+ <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
+ <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">0</NRCTotal>
+ <NRCComponents>
+ <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">0</AirframeEngAndDesign>
+ <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">0</DevSupportAndTesting>
+ <FlightTestAC>
+ <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">0</FlightTestACTotal>
+ <FlightTestACComponents>
+ <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">0</EngineAndAvionics>
+ <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">0</LaborManufacturing>
+ <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">0</MaterialManufacturing>
+ <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">0</Tooling>
+ <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">0</QualityControl>
+ </FlightTestACComponents>
+ </FlightTestAC>
+ <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">0</FlightTestOp>
+ <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
+ </NRCComponents>
+ </NonRecurringCosts>
+ <RecurringCosts Desc="Recurring Costs">
+ <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">0</RCTotal>
+ <RCComponents>
+ <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">0</Wing>
+ <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">0</Fuselage>
+ <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">0</Empennage>
+ <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">0</LandingGear>
+ <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">0</Pylons>
+ <PowerUnit Desc="Costs for all installed engines with systems without pylons">
+ <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">0</PowerUnitTotal>
+ <PowerUnitComponents>
+ <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">0</EquippedEngines>
+ <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">0</Nacelles>
+ <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">0</BleedAirSystem>
+ <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">0</FuelSystem>
+ </PowerUnitComponents>
+ </PowerUnit>
+ <Systems>
+ <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">0</SystemsTotal>
+ <SystemsComponents>
+ <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">0</APU>
+ <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">0</HydraulicSystem>
+ <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">0</AirConditioning>
+ <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">0</DeIcing>
+ <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">0</FireProtection>
+ <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">0</FlightControls>
+ <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">0</Instruments>
+ <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">0</AutomaticFlightSystem>
+ <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">0</Navigation>
+ <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">0</Communication>
+ <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">0</ElectricalSystem>
+ </SystemsComponents>
+ </Systems>
+ <Furnishings>
+ <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">0</FurnishingsTotal>
+ <FurnishingsComponents>
+ <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">0</Furnishing>
+ <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">0</FixedEmergencyOxygen>
+ <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">0</Lighting>
+ <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">0</WaterInstallation>
+ </FurnishingsComponents>
+ </Furnishings>
+ <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">0</OperatorsItems>
+ <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">0</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="">0</FlightsPerYear>
+ <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">0</SeatLoadFactor>
+ </OperatingScenario>
+ <DirectOperatingCosts>
+ <DOC_total Desc="Summe aller DOCComponents (s.u)">
+ <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">0</DOC_year>
+ <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</DOC_FH>
+ <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</DOC_flight>
+ <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</DOC_km>
+ <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</DOC_100ASK>
+ </DOC_total>
+ <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
+ <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">0</COC_year>
+ <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</COC_FH>
+ <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</COC_flight>
+ <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</COC_km>
+ <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</COC_100ASK>
+ </COC_total>
+ <DOCComponents Desc="DOC-Anteile in 100ASK">
+ <Charge Desc="Gebuehren pro 100ASK">
+ <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">0</ChargeTotal>
+ <ChargesComponents>
+ <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0</NavigationCharge>
+ <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0</LandingCharge>
+ <LandingChargeComponents>
+ <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/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</ChargeWithoutEmission>
+ </LandingChargeComponents>
+ <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0</GroundCharge>
+ </ChargesComponents>
+ </Charge>
+ <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0</Depreciation>
+ <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0</Insurance>
+ <Maintenance Desc="Wartungskosten">
+ <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0</MaintenanceTotal>
+ <MaintenanceComponents>
+ <Airframe Desc="Wartungskosten Airframe">
+ <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0</AirframeTotal>
+ <CostComponents>
+ <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
+ <ATA21 Desc="Environmental Control System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA21>
+ <ATA22 Desc="Autoflight">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA22>
+ <ATA23 Desc="Communications">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA23>
+ <ATA24 Desc="Electrical System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA24>
+ <ATA25 Desc="Furnishing">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA25>
+ <ATA26 Desc="Fire Protection">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA26>
+ <ATA27 Desc="Flight Control System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA27>
+ <ATA28 Desc="Fuel System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA28>
+ <ATA29 Desc="Hydraulic System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA29>
+ <ATA30 Desc="Ice and Rain Protection">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA30>
+ <ATA31 Desc="Instrumentation">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA31>
+ <ATA32 Desc="Landing Gear">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA32>
+ <ATA33 Desc="Lights">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA33>
+ <ATA34 Desc="Navigation">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA34>
+ <ATA35 Desc="Oxygen">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA35>
+ <ATA36 Desc="Pneumatic">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA36>
+ <ATA38 Desc="Water and Waste">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA38>
+ <ATA49 Desc="APU">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA49>
+ <ATA51 Desc="Structure">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA51>
+ <ATA52 Desc="Doors">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA52>
+ <ATA53 Desc="Fuselage">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA53>
+ <ATA54 Desc="Nacelles">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA54>
+ <ATA55 Desc="Stabilizers">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA55>
+ <ATA56 Desc="Windows">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA56>
+ <ATA57 Desc="Wings">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA57>
+ <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA99>
+ </AirframeComponents>
+ </Airframe>
+ <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0</Engine>
+ </MaintenanceComponents>
+ </Maintenance>
+ <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">0</Fuel>
+ <Crew Desc="Crew Kosten">
+ <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0</CrewTotal>
+ <CrewComponents>
+ <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</FlightCrew>
+ <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</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">0</IOC_year>
+ <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</IOC_FH>
+ <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</IOC_flight>
+ <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</IOC_km>
+ <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</IOC_100ASK>
+ </IOC_total>
+ </IndirectOperatingCosts>
+ </OperatingCosts>
+ <EndOfLifeCosts>
+ <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">0</EOLCTotal>
+ <EOLCTotalComponents>
+ <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">0</TransportToEoLSite>
+ <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">0</DisassemblyAndDismantling>
+ <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">0</Recycling>
+ <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">0</Incineration>
+ <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">0</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">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</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">0</HC>
+ </Development>
+ <Production>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</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">0</HC>
+ </Production>
+ <Operations>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</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">0</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">0</CO2>
+ <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</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">0</Total>
+ <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">0</TaxiTime>
+ <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0</TakeOffTime>
+ <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0</ClimbOutTime>
+ <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">0</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">0</CO2>
+ <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</PM10>
+ </LTO>
+ <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
+ <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0</PM10>
+ </Cruise>
+ </Mission>
+ </OperationComponents>
+ </Operations>
+ <EndOfLife>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</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">0</HC>
+ </EndOfLife>
+ </Emissions>
+ <CED Desc="Cumulative Energy Demand">
+ <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">0</CEDTotal>
+ <CEDComponents>
+ <Development Desc="Development" ToolLevel="1" Unit="MJ">0</Development>
+ <Production Desc="Production" ToolLevel="1" Unit="MJ">0</Production>
+ <Operations Desc="Operation" ToolLevel="1" Unit="MJ">0</Operations>
+ <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">0</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</ATR>
+ <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">0</AGTP>
+ <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">0</AGTP100>
+ <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">0</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</HC>
+ <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0</CO>
+ <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0</NOx>
+ <soot Desc="TF Russ" ToolLevel="1" Unit="-">0</soot>
+ </ToleranceFactors>
+ <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">0</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">
+ <DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
+ <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
+ <TOFL_Design Desc="Design takeoff distance (Balanced Field Length) at Sea Level with MTOM and (ISA + deltaISA)-Conditions" Unit="m">2122</TOFL_Design>
+ <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+deltaISA)" 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="Needed runway length at Sea Level with MLM and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" Unit="m">2387</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">
+ <DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
+ <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>
+ <FrictionCoefficient Default="0.03" Desc="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">0.03</FrictionCoefficient>
+ <BrakingCoefficient Default="0.34189" Desc="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">0.34189</BrakingCoefficient>
+ </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>
+ <SkinThickness Default="0" Desc="Skin thickness of profiles" Unit="m">0</SkinThickness>
+ </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>
+ <NumberOfPropulsors Desc="Number of powertrains" ToolLevel="1">2</NumberOfPropulsors>
+ <Propulsor ID="1">
+ <TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
+ <PropulsorPosition>
+ <ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
+ <yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">1</yPosition>
+ <xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
+ </PropulsorPosition>
+ </Propulsor>
+ <Propulsor ID="2">
+ <TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
+ <PropulsorPosition>
+ <ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
+ <yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">-1</yPosition>
+ <xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
+ </PropulsorPosition>
+ </Propulsor>
+ <FuelDensity Desc="Density of fuel" 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="-">2.4</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>
+ <NormalManeuver Default="1.1" Desc="Normal used load factor for maneuvers (e.g. flare)">1.1</NormalManeuver>
+ </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>
+ <OperatingCondition>
+ <HLFConlyForCruise>1</HLFConlyForCruise>
+ <MinMachForHLFCActivation>0.78</MinMachForHLFCActivation>
+ </OperatingCondition>
+ </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>
+ <VariableCamber Desc="Aircraft has VC segments">0</VariableCamber>
+ </Technology>
+ </DesignSpecification>
+</AcftExchangeFile>
diff --git a/scripts/document_aircraft_xml.py b/scripts/document_aircraft_xml.py
new file mode 100644
index 0000000..5602803
--- /dev/null
+++ b/scripts/document_aircraft_xml.py
@@ -0,0 +1,233 @@
+#!python
+# Copyright (c) 2023 S. Oberschwendtner.
+#
+#
+# This program is free software: you can redistribute it and/or modify
+# it under the terms of the GNU General Public License as published by
+# the Free Software Foundation, either version 3 of the License, or
+# (at your option) any later version.
+#
+# This program is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
+# GNU General Public License for more details.
+#
+# You should have received a copy of the GNU General Public License
+# along with this program. If not, see <https://www.gnu.org/licenses/>.
+
+"""! @brief Script for converting an aircraft XML file to a content page."""
+##
+# @file document_aircraft_xml.py
+#
+# @brief Script for converting an aircraft XML file to a content page for the UNICADO homepage.
+#
+# @section description_document_aircraft_xml Description
+# This script parse the entries of an aircraft XML file and extracts
+# the entries and documents them using their description tags.
+# The output is a markdown file which can be used for the documentation.
+#
+# @section libraries_document_aircraft_xml Libraries/Modules
+# - argparse standard library (https://docs.python.org/3/library/argparse.html)
+# - Parser for command-line options, arguments and sub-commands.
+# - xml standard library (https://docs.python.org/3/library/xml.html)
+# - XML Processing Modules.
+# - pathlib standard library (https://docs.python.org/3/library/pathlib.html)
+# - Object-oriented filesystem paths.
+#
+# @section notes_document_aircraft_xml Notes
+# - None.
+#
+# @section todo_document_aircraft_xml TODO
+# - None.
+#
+# @section authors_document_aircraft_xml Author(s)
+# - Created by S. Oberschwendtner on 19/09/2023.
+
+# === Imports ===
+import argparse
+import xml.etree.ElementTree as ET
+from pathlib import Path
+
+# === Configuration ===
+# Define the format of the output
+FORMAT = {
+ "Header": "# {:s}\n> **Description**: {:s}\n",
+ "Unit": "> **Unit**: {:s}\n",
+ "TableHeader": "| Relative XML Path | Unit | Description |\n|:---|:---:|:---|",
+ "Table": "| <nobr>`{:s}` | *{:s}* | {:s} |",
+}
+
+# Which keys are used in the XML attributes for which information
+KEYS = {
+ "Description": "Desc",
+ "Unit": "Unit",
+}
+
+
+# === Classes ===
+class Page:
+ """Class for a page.
+
+ A page is one top section of the aircraft XML file.
+ """
+
+ @property
+ def max_level_reached(self) -> bool:
+ """Returns whether the maximum level has been reached."""
+ return self.current_level >= self.max_header_level
+
+ def __init__(self, title, max_level):
+ """Constructor of the class.
+
+ Args:
+ title (str): Title of the page.
+ max_level (int): Maximum level of the headers.
+ """
+ self.title = title
+ self.max_header_level = max_level
+ self.current_level = 0
+ self.table_started = False
+ self.current_path = Path(".")
+ self.sections = [[]]
+
+ def create(self, node: ET.Element):
+ """Creates the page from the given node.
+
+ This function adds all subnodes of the given node to the page.
+ It recursively calls itself for all subnodes.
+
+ It does not add sections which are already present in the current level.
+
+ Args:
+ node (ET.Element): Node to start from.
+ """
+ # Only add the header if it was not already added at this level
+ if node.tag in self.sections[self.current_level]:
+ return
+
+ # Check whether the current entry can be a header
+ if not self.max_level_reached:
+ self.sections[self.current_level].append(node.tag)
+ self.make_header_entry(node)
+ self.current_path = Path(node.tag)
+ else:
+ self.current_path /= node.tag
+
+ # Loop through the children and group single entries in a table
+ for child in node:
+ if len(child) == 0:
+ self.make_table_entry(child)
+
+ # Add a new level of sections
+ self.current_level += 1
+ self.sections.append([])
+
+ # Loop again and add the subnodes
+ for child in node:
+ if len(child) > 0:
+ self.create(child)
+
+ # Decrease the level again when finished
+ self.current_level -= 1
+ self.sections.pop()
+ self.current_path = self.current_path.parent
+
+ def make_header_entry(self, node: ET.Element):
+ """Creates a header entry.
+
+ Args:
+ node (ET.Element): The current node element.
+ """
+ # Reset the table when creating a new header
+ self.table_started = False
+
+ # Create the header with description
+ print(
+ "\n"
+ + self.current_level * "#"
+ + FORMAT["Header"].format(
+ node.tag, node.attrib.get(KEYS["Description"], "None")
+ )
+ )
+
+ # Try to add a unit description
+ try:
+ print(FORMAT["Unit"].format(node.attrib[KEYS["Unit"]]))
+ except KeyError:
+ pass
+
+ def make_table_entry(self, node: ET.Element):
+ """Creates a table entry.
+
+ Args:
+ node (ET.Element): The current node element.
+ """
+ # Check if the table has already been started
+ if not self.table_started:
+ self.table_started = True
+ print(FORMAT["TableHeader"])
+
+ # Since we use pathlib for convenience, we need to convert it to a string
+ # and replace the backslashes with forward slashes
+ path_name = str(self.current_path / node.tag).replace("\\", "/")
+
+ # Create the header with description
+ print(
+ FORMAT["Table"].format(
+ path_name,
+ node.attrib.get(KEYS["Unit"], "-"),
+ node.attrib.get(KEYS["Description"], "None"),
+ )
+ )
+
+
+# === Main ===
+def main():
+ """
+ Main function of the script.
+ """
+ # Create argument parser
+ parser = argparse.ArgumentParser(
+ description="Converts an aircraft XML file to a markdown file. The output is streamed to stdout and can be piped to a file."
+ )
+
+ # Add the filename argument
+ parser.add_argument(
+ "filename", metavar="filename", type=str, help="The XML file to convert."
+ )
+
+ # Add the layout arguments
+ parser.add_argument(
+ "--title",
+ metavar="title",
+ type=str,
+ help="The title of the output page. This also sets the root node which is used to create the document.",
+ )
+ parser.add_argument(
+ "--level",
+ metavar="level",
+ type=int,
+ help="The maximum level nodes to be used as headers.",
+ )
+
+ # Parse the arguments
+ args = parser.parse_args()
+
+ # Read the XML file
+ tree = ET.parse(args.filename)
+ root = tree.getroot()
+
+ # Get the configuration parameters
+ page = Page(args.title, args.level)
+ node = root.find(page.title)
+
+ # Check whether the node exists
+ if node is None:
+ raise Warning("Could not find node with title '" + page.title + "'")
+
+ # Start creating the page
+ page.create(node)
+
+
+if __name__ == "__main__":
+ main()
--
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