From 858aa67a1fe3bfdfbe563c9e2eabd05fa55104e5 Mon Sep 17 00:00:00 2001
From: Kristina Mazur <kristina.mazur@tum.de>
Date: Tue, 3 Dec 2024 15:11:38 +0100
Subject: [PATCH] Update pipeline creating documentation and delete script for
acXML parsing
---
.gitlab-ci.yml | 39 +-
scripts/CSR-02.xml | 3767 ------------------------------
scripts/document_aircraft_xml.py | 233 --
3 files changed, 13 insertions(+), 4026 deletions(-)
delete mode 100644 scripts/CSR-02.xml
delete mode 100644 scripts/document_aircraft_xml.py
diff --git a/.gitlab-ci.yml b/.gitlab-ci.yml
index 4a05c73..41dbc60 100644
--- a/.gitlab-ci.yml
+++ b/.gitlab-ci.yml
@@ -28,18 +28,20 @@ doxygen:
before_script:
- apk update && apk --no-cache add git doxygen graphviz ttf-freefont texmf-dist texmf-dist-latexextra texlive texlive-dvi
script:
- # libaries
- - git clone --recurse-submodules https://gitlab-ci-token:${CI_JOB_TOKEN}@git.rwth-aachen.de/unicado/libraries
- - cd libraries/aircraftGeometry2/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
+ # clone repos
+ - git clone https://gitlab-ci-token:${CI_JOB_TOKEN}@git.rwth-aachen.de/unicado/aircraft-design
+ - cd aircraft-design
+ - git clone --recurse-submodules https://gitlab-ci-token:${CI_JOB_TOKEN}@git.rwth-aachen.de/unicado/libraries libs/
+ # create aircraft design documentation
+ - cd propulsion_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
+ - cd ../../wing_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
+ - cd ../../empennage_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
+ - cd ../../ecological_assessment/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
+ # create libraries documentation
+ - cd ../../libs/aircraftGeometry2/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
- cd ../../engine/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
- cd $CI_PROJECT_DIR
- # aircraft design
- - git clone --recurse-submodules https://gitlab-ci-token:${CI_JOB_TOKEN}@git.rwth-aachen.de/unicado/aircraft-design
- - cd aircraft-design/propulsion_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
- - cd ../../aircraft-design/wing_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
- - cd ../../aircraft-design/empennage_design/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
- - cd ../../aircraft-design/ecological_assessment/doc/ && ( cat Doxyfile ; echo "OUTPUT_DIRECTORY = $CI_PROJECT_DIR/docs/documentation/" ) | doxygen -
-
+
artifacts:
paths:
- $CI_PROJECT_DIR/docs/documentation
@@ -60,22 +62,7 @@ pages:
before_script:
- pip install pipenv
- pipenv install
- script:
- - mkdir $CI_PROJECT_DIR/docs/aircraft-xml
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title General --level 1 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/general.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title MassesAndLoadings --level 3 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/masses.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Geometry --level 6 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/geometry.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Structure --level 2 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/structure.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Accommodation --level 2 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/accommodation.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Propulsion --level 3 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/propulsion.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Systems --level 2 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/systems.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Aerodynamics --level 2 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/aerodynamics.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title StabilityAndControlCharacteristics --level 2 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/stability.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Performance --level 4 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/performance.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title MonetaryValues --level 4 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/monetary.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title EcologicalValues --level 4 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/ecological.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title Requirements --level 3 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/requirements.md
- - python $CI_PROJECT_DIR/scripts/document_aircraft_xml.py --title DesignSpecification --level 4 $CI_PROJECT_DIR/scripts/CSR-02.xml > $CI_PROJECT_DIR/docs/aircraft-xml/specification.md
+ script:cmks
- pipenv run mkdocs build --site-dir $CI_PROJECT_DIR/public
needs:
- doxygen
diff --git a/scripts/CSR-02.xml b/scripts/CSR-02.xml
deleted file mode 100644
index e79520e..0000000
--- a/scripts/CSR-02.xml
+++ /dev/null
@@ -1,3767 +0,0 @@
-<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
deleted file mode 100644
index 5602803..0000000
--- a/scripts/document_aircraft_xml.py
+++ /dev/null
@@ -1,233 +0,0 @@
-#!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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