diff --git a/.gitignore b/.gitignore
new file mode 100644
index 0000000000000000000000000000000000000000..d9dd1e071300d75ae4e1ef72d25fcd677f1b1398
--- /dev/null
+++ b/.gitignore
@@ -0,0 +1,5 @@
+# Ignore generated Doxygen docs in modules folder
+docs/modules/**/
+
+# Ignore the local docs of the AcXML
+docs/aircraft-xml/
diff --git a/.gitlab-ci.yml b/.gitlab-ci.yml
index 5308c4ef57fefcb038b70a196dc9aa29697dba1b..d13b0e879bbca24271a9b93ed001000359501631 100644
--- a/.gitlab-ci.yml
+++ b/.gitlab-ci.yml
@@ -15,17 +15,61 @@
# along with this program. If not, see <https://www.gnu.org/licenses/>.
# === Configure pipeline ===
-image: python:latest
+stages:
+ - build
+ - deploy
+
+# === Build the doxygen documentation ===
+doxygen:
+ image: alpine:latest
+ stage: build
+ tags:
+ - documentation
+ before_script:
+ - apk update && apk --no-cache add git doxygen graphviz ttf-freefont texmf-dist texmf-dist-latexextra texlive texlive-dvi
+ script:
+ - git clone -b feature-aircraftGeometry2 --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/modules/" ) | doxygen -
+ artifacts:
+ paths:
+ - $CI_PROJECT_DIR/docs/modules
+ rules:
+ - if: '$CI_COMMIT_BRANCH == $CI_DEFAULT_BRANCH'
+ when: on_success
+ - if: '$CI_COMMIT_BRANCH != $CI_DEFAULT_BRANCH'
+ when: manual
+
+# === Build and deploy the website ===
pages:
+ image: python:latest
stage: deploy
tags:
- documentation
+ before_script:
+ - pip install pipenv
+ - pipenv install
script:
- - pip install mkdocs-material
- - mkdocs build --site-dir public
+ - 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
+ - pipenv run mkdocs build --site-dir $CI_PROJECT_DIR/public
+ needs:
+ - doxygen
artifacts:
paths:
- - public
+ - $CI_PROJECT_DIR/public
rules:
- if: '$CI_COMMIT_BRANCH == $CI_DEFAULT_BRANCH'
when: on_success
diff --git a/Pipfile b/Pipfile
new file mode 100644
index 0000000000000000000000000000000000000000..49fa86bd287ebe858f8ea4c6f44ad91385aa983b
--- /dev/null
+++ b/Pipfile
@@ -0,0 +1,14 @@
+[[source]]
+url = "https://pypi.org/simple"
+verify_ssl = true
+name = "pypi"
+
+[packages]
+mkdocs = "*"
+mkdocs-material = "*"
+mkdocs-glightbox = "*"
+
+[dev-packages]
+
+[requires]
+python_version = "3.11"
diff --git a/Pipfile.lock b/Pipfile.lock
new file mode 100644
index 0000000000000000000000000000000000000000..146ff6db1761d011930198a429478ffbd475a172
--- /dev/null
+++ b/Pipfile.lock
@@ -0,0 +1,557 @@
+{
+ "_meta": {
+ "hash": {
+ "sha256": "5fea7d31e7a99ffb6bc6be5d229a52f08658f807b7a75251742107aff366537a"
+ },
+ "pipfile-spec": 6,
+ "requires": {
+ "python_version": "3.11"
+ },
+ "sources": [
+ {
+ "name": "pypi",
+ "url": "https://pypi.org/simple",
+ "verify_ssl": true
+ }
+ ]
+ },
+ "default": {
+ "babel": {
+ "hashes": [
+ "sha256:33e0952d7dd6374af8dbf6768cc4ddf3ccfefc244f9986d4074704f2fbd18900",
+ "sha256:7077a4984b02b6727ac10f1f7294484f737443d7e2e66c5e4380e41a3ae0b4ed"
+ ],
+ "markers": "python_version >= '3.7'",
+ "version": "==2.13.1"
+ },
+ "certifi": {
+ "hashes": [
+ "sha256:539cc1d13202e33ca466e88b2807e29f4c13049d6d87031a3c110744495cb082",
+ "sha256:92d6037539857d8206b8f6ae472e8b77db8058fec5937a1ef3f54304089edbb9"
+ ],
+ "markers": "python_version >= '3.6'",
+ "version": "==2023.7.22"
+ },
+ "charset-normalizer": {
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diff --git a/README.md b/README.md
index be3fcf97378353c5515a1f5b83e6b3f4bcaa09be..479a9d14ded004c8792b2d3a7c565f2473ab5e94 100644
--- a/README.md
+++ b/README.md
@@ -7,7 +7,7 @@ We are using `mkdocs` as the static site generator to generate the website from
You can preview the website after cloning it. First you need to install `mkdocs` and the used theme by:
```sh
-pip install mkdocs mkdocs-material
+pip install mkdocs mkdocs-material mkdocs-glightbox
```
Then you can change the directory to the repository and run
@@ -17,8 +17,56 @@ mkdocs serve
This will start a local webserver which you can access with your webbrowser and preview the website.
+### with pipenv
+You can also start the server inside a virtual environment using `pipenv`:
+```sh
+pipenv run mkdocs serve
+```
+
## Further Documentation
For features of the site generator and its theme please refer to their excellent documentation:
- [⤷ MkDocs](https://www.mkdocs.org/user-guide/)
-- [⤷ MkDocs Material](https://squidfunk.github.io/mkdocs-material/)
\ No newline at end of file
+- [⤷ MkDocs Material](https://squidfunk.github.io/mkdocs-material/)
+
+## Page Template
+The pages are written in plain *markdown*.
+The site generator has the option the extract some meta data from the content.
+A template might look like this:
+```
+---
+title: Displayed Title of Page
+summary: Summary of the page content.
+authors:
+ - Author 1
+ - Author 2
+date: yyyy-mm-dd
+---
+# MyPage
+
+<Content goes here>
+```
+
+# Tools
+The documentation page uses some custom tools to enable a seamless continuous documentation:
+
+## document_aircraft_xml.py
+> Script
+
+This script is used to document the aircraft exchange file.
+It parses the XML file and creates the documentation for each node using its description.
+
+The usage is explained in the output when calling the script with the `--help` option:
+```sh
+usage: document_aircraft_xml.py [-h] [--title title] [--level level] filename
+
+Converts an aircraft XML file to a markdown file. The output is streamed to stdout and can be piped to a file.
+
+positional arguments:
+ filename The XML file to convert.
+
+options:
+ -h, --help show this help message and exit
+ --title title The title of the output page. This also sets the root node which is used to create the document.
+ --level level The maximum level nodes to be used as headers.
+```
diff --git a/docs/assets/css/unicado.css b/docs/assets/css/unicado.css
new file mode 100644
index 0000000000000000000000000000000000000000..489f70ee5aaadec5284963a265303ac495affcd7
--- /dev/null
+++ b/docs/assets/css/unicado.css
@@ -0,0 +1,28 @@
+.grid-container {
+ grid-gap: .4rem;
+ display: grid;
+ grid-template-columns: repeat(auto-fit,minmax(16rem,1fr));
+ margin: 1em 0;
+}
+
+.grid-item {
+ border: .05rem solid var(--md-default-fg-color--lightest);
+ border-radius: .1rem;
+ display: block;
+ margin: 0;
+ padding: .8rem;
+ transition: border .25s,box-shadow .25s;
+}
+
+.grid-item:where(:hover, :focus) {
+ border-color: #0000;
+ box-shadow: var(--md-shadow-z2);
+}
+
+.overview-item {
+ min-height: 240px;
+}
+
+.overview-img {
+ width: 200px;
+}
\ No newline at end of file
diff --git a/docs/assets/images/banner.png b/docs/assets/images/banner.png
new file mode 100644
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--- /dev/null
+++ b/docs/assets/images/banner.png
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:5ac8b569949a92d73185474a331f292f9a293c73d3df76ba899b1d64e9a2d285
+size 2582463
diff --git a/docs/assets/images/logos/bmwk.png b/docs/assets/images/logos/bmwk.png
new file mode 100644
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--- /dev/null
+++ b/docs/assets/images/logos/bmwk.png
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:555f9bf46a20eac600d935819842d89968800211cc4e91d99411fd5687586927
+size 26109
diff --git a/docs/assets/images/icon.png b/docs/assets/images/logos/unicado-icon.png
similarity index 100%
rename from docs/assets/images/icon.png
rename to docs/assets/images/logos/unicado-icon.png
diff --git a/docs/assets/images/logo.png b/docs/assets/images/logos/unicado.png
similarity index 100%
rename from docs/assets/images/logo.png
rename to docs/assets/images/logos/unicado.png
diff --git a/docs/assets/images/modules/aerodynamics.svg b/docs/assets/images/modules/aerodynamics.svg
new file mode 100644
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--- /dev/null
+++ b/docs/assets/images/modules/aerodynamics.svg
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+<?xml version="1.0" encoding="UTF-8" standalone="no"?>
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+
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+ width="1080"
+ height="1080"
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+ xml:space="preserve"
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+ xmlns:svg="http://www.w3.org/2000/svg"><defs
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+<!-- Created with Inkscape (http://www.inkscape.org/) -->
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+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,568.75 L81.25,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,568.75 L81.25,556.75 M81.25,105.26 L81.25,117.26 '/> <g transform="translate(81.25,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
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+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M178.75,568.75 L178.75,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M178.75,568.75 L178.75,556.75 M178.75,105.26 L178.75,117.26 '/> <g transform="translate(178.75,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0.01</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M276.25,568.75 L276.25,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M276.25,568.75 L276.25,556.75 M276.25,105.26 L276.25,117.26 '/> <g transform="translate(276.25,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0.02</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M373.74,568.75 L373.74,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M373.74,568.75 L373.74,556.75 M373.74,105.26 L373.74,117.26 '/> <g transform="translate(373.74,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0.03</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M471.24,568.75 L471.24,556.75 M471.24,394.75 L471.24,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M471.24,568.75 L471.24,556.75 M471.24,105.26 L471.24,117.26 '/> <g transform="translate(471.24,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0.04</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M568.74,568.75 L568.74,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M568.74,568.75 L568.74,556.75 M568.74,105.26 L568.74,117.26 '/> <g transform="translate(568.74,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 0.05</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,105.26 L81.25,568.75 L568.74,568.75 L568.74,105.26 L81.25,105.26 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(34.42,337.01) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="12.8" dy="4.80px">L</tspan><tspan font-size="16.0" dy="-4.80"></tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(324.99,633.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="12.8" dy="4.80px">D, total</tspan><tspan font-size="16.0" dy="-4.80"></tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M453.25,556.75 L453.25,394.75 L557.54,394.75 L557.54,556.75 L453.25,556.75 Z '/></g>
+ <g id="gnuplot_plot_1a" ><title>Ma 0.20</title>
+<g fill="none" color="white" stroke="black" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,407.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.20</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ </g>
+ <g id="gnuplot_plot_2a" ><title>Ma 0.50</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,425.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.50</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(105, 105, 105)' stroke-dasharray=' 5,8' d='M520.37,421.75 L549.15,421.75 M291.04,568.75 L286.35,560.47 L282.14,552.20 L278.43,543.92 L275.22,535.64 L272.50,527.37
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+ </g>
+ <g id="gnuplot_plot_3a" ><title>Ma 0.58</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,443.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.58</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ </g>
+ <g id="gnuplot_plot_4a" ><title>Ma 0.68</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,461.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.68</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(211, 211, 211)' stroke-dasharray=' 8,4,2,4' d='M520.37,457.75 L549.15,457.75 M306.33,568.75 L301.80,560.47 L297.75,552.20 L294.18,543.92 L291.09,535.64 L288.45,527.37
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+ </g>
+ <g id="gnuplot_plot_5a" ><title>Ma 0.73</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,479.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.73</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(112, 128, 144)' stroke-dasharray=' 9,4,1,4,1,4' d='M520.37,475.75 L549.15,475.75 M305.50,568.75 L300.99,560.47 L296.95,552.20 L293.41,543.92 L290.31,535.64 L287.69,527.37
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+ </g>
+ <g id="gnuplot_plot_6a" ><title>Ma 0.76</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,497.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.76</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(159, 182, 205)' stroke-dasharray='20.0,10.0' d='M520.37,493.75 L549.15,493.75 M305.13,568.75 L300.66,560.47 L296.66,552.20 L293.14,543.92 L290.09,535.64 L287.51,527.37
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+ '/></g>
+ </g>
+ <g id="gnuplot_plot_7a" ><title>Ma 0.78</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,515.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.78</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(198, 226, 255)' stroke-dasharray='10.0,10.0' d='M520.37,511.75 L549.15,511.75 M305.23,568.75 L300.83,560.47 L296.90,552.20 L293.45,543.92 L290.48,535.64 L287.98,527.37
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+ '/></g>
+ </g>
+ <g id="gnuplot_plot_8a" ><title>Ma 0.79</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,533.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.79</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb( 82, 139, 139)' stroke-dasharray='2.0,5.0,20.0,10.0' d='M520.37,529.75 L549.15,529.75 M305.53,568.75 L301.19,560.47 L297.33,552.20 L293.96,543.92 L291.07,535.64 L288.65,527.37
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+ </g>
+ <g id="gnuplot_plot_9a" ><title>Ma 0.83</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,551.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.83</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M1137.49,568.75 L1137.49,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M1137.49,568.75 L1137.49,556.75 M1137.49,105.26 L1137.49,117.26 '/> <g transform="translate(1137.49,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 1</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M1178.12,568.75 L1178.12,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M1178.12,568.75 L1178.12,556.75 M1178.12,105.26 L1178.12,117.26 '/> <g transform="translate(1178.12,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 1.1</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M1218.74,568.75 L1218.74,105.26 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M1218.74,568.75 L1218.74,556.75 M1218.74,105.26 L1218.74,117.26 '/> <g transform="translate(1218.74,597.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" > 1.2</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,105.26 L731.25,568.75 L1218.74,568.75 L1218.74,105.26 L731.25,105.26 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(695.62,337.01) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >L/D</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(974.99,633.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="12.8" dy="4.80px">L</tspan><tspan font-size="16.0" dy="-4.80"></tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+ <g id="gnuplot_plot_1b" ><title>Ma 0.20</title>
+<g fill="none" color="white" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb( 0, 0, 0)' d='M762.63,568.75 L771.87,535.17 L782.03,499.07 L792.19,464.01 L802.34,430.26 L812.50,398.03 L822.65,367.50 L832.81,338.84
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+ </g>
+ <g id="gnuplot_plot_2b" ><title>Ma 0.50</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(105, 105, 105)' stroke-dasharray=' 5,8' d='M762.15,568.75 L771.87,532.89 L782.03,496.24 L792.19,460.65 L802.34,426.39 L812.50,393.66 L822.65,362.67 L832.81,333.57
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+ </g>
+ <g id="gnuplot_plot_3b" ><title>Ma 0.58</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(190, 190, 190)' stroke-dasharray=' 2,4' d='M763.05,568.75 L771.87,537.03 L782.03,501.23 L792.19,466.39 L802.34,432.74 L812.50,400.50 L822.65,369.88 L832.81,341.04
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+ </g>
+ <g id="gnuplot_plot_4b" ><title>Ma 0.68</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(211, 211, 211)' stroke-dasharray=' 8,4,2,4' d='M764.81,568.75 L771.87,544.63 L782.03,510.58 L792.19,477.37 L802.34,445.22 L812.50,414.32 L822.65,384.85 L832.81,356.97
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+ </g>
+ <g id="gnuplot_plot_5b" ><title>Ma 0.73</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(112, 128, 144)' stroke-dasharray=' 9,4,1,4,1,4' d='M764.67,568.75 L771.87,544.06 L782.03,509.84 L792.19,476.48 L802.34,444.17 L812.50,413.11 L822.65,383.49 L832.81,355.48
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+ </g>
+ <g id="gnuplot_plot_6b" ><title>Ma 0.76</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(159, 182, 205)' stroke-dasharray='20.0,10.0' d='M764.69,568.75 L771.87,544.18 L782.03,510.06 L792.19,476.82 L802.34,444.69 L812.50,413.85 L822.65,384.51 L832.81,356.82
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+ </g>
+ <g id="gnuplot_plot_7b" ><title>Ma 0.78</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(198, 226, 255)' stroke-dasharray='10.0,10.0' d='M764.91,568.75 L771.87,545.16 L782.03,511.44 L792.19,478.67 L802.34,447.08 L812.50,416.85 L822.65,388.17 L832.81,361.21
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+ L1005.46,257.92 L1015.62,276.05 L1025.78,296.49 L1035.93,318.87 '/></g>
+ </g>
+ <g id="gnuplot_plot_8b" ><title>Ma 0.79</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb( 82, 139, 139)' stroke-dasharray='2.0,5.0,20.0,10.0' d='M765.15,568.75 L771.87,546.21 L782.03,512.87 L792.19,480.53 L802.34,449.42 L812.50,419.71 L822.65,391.60 L832.81,365.24
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+ L1005.46,272.70 L1015.62,291.29 '/></g>
+ </g>
+ <g id="gnuplot_plot_9b" ><title>Ma 0.83</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(121, 205, 205)' stroke-dasharray='2.0,5.0,2.0,5.0,10.0,10.0' d='M768.15,568.75 L771.87,557.49 L782.03,527.72 L792.19,499.19 L802.34,472.08 L812.50,446.52 L822.65,422.63 L832.81,400.53
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+ L924.21,290.76 L934.37,289.29 '/></g>
+ </g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,105.26 L731.25,568.75 L1218.74,568.75 L1218.74,105.26 L731.25,105.26 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(974.99,74.46)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >L/D Polar</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,1218.75 L568.74,1218.75 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,1218.75 L93.25,1218.75 M568.74,1218.75 L556.74,1218.75 '/> <g transform="translate(70.05,1223.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.8</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,1141.50 L411.30,1141.50 M557.54,1141.50 L568.74,1141.50 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,1141.50 L93.25,1141.50 M568.74,1141.50 L556.74,1141.50 '/> <g transform="translate(70.05,1146.70)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.4</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,1064.25 L411.30,1064.25 M557.54,1064.25 L568.74,1064.25 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,1064.25 L93.25,1064.25 M568.74,1064.25 L556.74,1064.25 '/> <g transform="translate(70.05,1069.45)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.0</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,987.00 L568.74,987.00 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,987.00 L93.25,987.00 M568.74,987.00 L556.74,987.00 '/> <g transform="translate(70.05,992.20)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.4</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,909.75 L568.74,909.75 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,909.75 L93.25,909.75 M568.74,909.75 L556.74,909.75 '/> <g transform="translate(70.05,914.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.8</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M81.25,832.50 L568.74,832.50 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ <text><tspan font-family="Times" >1.6</tspan></text>
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+ <g transform="translate(31.80,987.00) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="14.00" text-anchor="middle">
+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="11.2" dy="4.20px">L</tspan><tspan font-size="14.0" dy="-4.20"></tspan></text>
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+ <text><tspan font-family="Times" >AoA [deg]</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.20</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.58</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.68</tspan></text>
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+ L410.31,885.61 L417.58,880.78 '/></g>
+ </g>
+ <g id="gnuplot_plot_6c" ><title>Ma 0.76</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1111.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.76</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(159, 182, 205)' stroke-dasharray='20.0,10.0' d='M520.37,1107.75 L549.15,1107.75 M81.25,1104.22 L83.23,1102.87 L90.37,1098.05 L97.48,1093.22 L104.61,1088.39 L111.75,1083.56
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+ </g>
+ <g id="gnuplot_plot_7c" ><title>Ma 0.78</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1129.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.78</tspan></text>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ </g>
+ <g id="gnuplot_plot_8c" ><title>Ma 0.79</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1147.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.79</tspan></text>
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+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ '/></g>
+ </g>
+ <g id="gnuplot_plot_9c" ><title>Ma 0.83</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1165.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Ma 0.83</tspan></text>
+ </g>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(121, 205, 205)' stroke-dasharray='2.0,5.0,2.0,5.0,10.0,10.0' d='M520.37,1161.75 L549.15,1161.75 M81.25,1105.99 L85.57,1102.87 L92.29,1098.05 L99.01,1093.22 L105.73,1088.39 L112.41,1083.56
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+ </g>
+ <g id="gnuplot_plot_10c" ><title>LILI (inc)</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1183.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >LILI (inc)</tspan></text>
+ </g>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <use xlink:href='#gpPt0' transform='translate(81.25,1098.05) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(150.89,1061.55) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(220.53,1025.05) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(290.17,988.54) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(359.82,952.24) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(429.46,916.12) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(499.10,880.40) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(568.74,844.09) scale(4.50)' color='rgb( 0, 0, 0)'/>
+ <use xlink:href='#gpPt0' transform='translate(534.76,1179.75) scale(4.50)' color='rgb( 0, 0, 0)'/>
+</g>
+ </g>
+ <g id="gnuplot_plot_11c" ><title>LILI (Ma 0.78)</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(511.98,1201.65)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >LILI (Ma 0.78)</tspan></text>
+ </g>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <use xlink:href='#gpPt0' transform='translate(81.25,1104.81) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(150.89,1056.78) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(220.53,1008.63) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(290.17,960.54) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(359.82,912.45) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(429.46,865.33) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(499.10,817.05) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(568.74,768.77) scale(4.50)' color='rgb(105, 105, 105)'/>
+ <use xlink:href='#gpPt0' transform='translate(534.76,1197.75) scale(4.50)' color='rgb(105, 105, 105)'/>
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+ </g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M81.25,755.25 L81.25,1218.75 L568.74,1218.75 L568.74,755.25 L81.25,755.25 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(324.99,741.25)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >Lift Polar</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,1218.75 L1218.74,1218.75 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,1218.75 L743.25,1218.75 M1218.74,1218.75 L1206.74,1218.75 '/> <g transform="translate(720.05,1223.95)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.4</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,1160.81 L742.45,1160.81 M888.69,1160.81 L1218.74,1160.81 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,1160.81 L743.25,1160.81 M1218.74,1160.81 L1206.74,1160.81 '/> <g transform="translate(720.05,1166.01)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.3</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,1102.87 L742.45,1102.87 M888.69,1102.87 L1218.74,1102.87 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,1102.87 L743.25,1102.87 M1218.74,1102.87 L1206.74,1102.87 '/> <g transform="translate(720.05,1108.07)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.2</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,1044.94 L742.45,1044.94 M888.69,1044.94 L1218.74,1044.94 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,1044.94 L743.25,1044.94 M1218.74,1044.94 L1206.74,1044.94 '/> <g transform="translate(720.05,1050.14)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >-0.1</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,987.00 L1218.74,987.00 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,987.00 L743.25,987.00 M1218.74,987.00 L1206.74,987.00 '/> <g transform="translate(720.05,992.20)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.0</tspan></text>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,929.06 L1218.74,929.06 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,929.06 L743.25,929.06 M1218.74,929.06 L1206.74,929.06 '/> <g transform="translate(720.05,934.26)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.1</tspan></text>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,871.12 L1218.74,871.12 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,871.12 L743.25,871.12 M1218.74,871.12 L1206.74,871.12 '/> <g transform="translate(720.05,876.32)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.2</tspan></text>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
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+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,813.19 L1218.74,813.19 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,813.19 L743.25,813.19 M1218.74,813.19 L1206.74,813.19 '/> <g transform="translate(720.05,818.39)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.3</tspan></text>
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+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
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+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,755.25 L1218.74,755.25 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M731.25,755.25 L743.25,755.25 M1218.74,755.25 L1206.74,755.25 '/> <g transform="translate(720.05,760.45)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.4</tspan></text>
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+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M731.25,1218.75 L731.25,755.25 '/></g>
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+ <text><tspan font-family="Times" > 1.2</tspan></text>
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+ <g transform="translate(681.80,987.00) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="14.00" text-anchor="middle">
+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="11.2" dy="4.20px">M</tspan><tspan font-size="14.0" dy="-4.20"></tspan></text>
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+ <text><tspan font-family="Times" >C</tspan><tspan font-family="Times" font-size="11.2" dy="4.20px">L</tspan><tspan font-size="14.0" dy="-4.20"></tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.50</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.58</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.68</tspan></text>
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+ <text><tspan font-family="Times" >Ma 0.73</tspan></text>
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+ <text><tspan font-family="Times" >Gear</tspan></text>
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+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ <text><tspan font-family="Times" >Propulsion</tspan></text>
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+</g>
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+</g>
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+ <text><tspan font-family="Times" >Systems</tspan></text>
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+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M577.77,205.00 L577.77,24.01 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
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+ <path stroke='black' d='M577.77,205.00 L577.77,193.00 M577.77,24.01 L577.77,36.01 '/> <g transform="translate(553.44,303.88) rotate(-45)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="start">
+ <text><tspan font-family="Times" >not Alloc</tspan></text>
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+</g>
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+ <path stroke='black' d='M89.60,24.01 L89.60,205.00 L638.79,205.00 L638.79,24.01 L89.60,24.01 Z '/></g>
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+ <g transform="translate(29.60,114.51) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >Mass/OME, %</tspan></text>
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+ <g transform="translate(536.62,210.03)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Planform (old)</tspan></text>
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+ <path stroke='black' d='M65.00,466.99 L77.00,466.99 '/> <g transform="translate(53.80,472.19)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >0.5</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,447.69 L584.99,447.69 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,447.69 L77.00,447.69 '/> <g transform="translate(53.80,452.89)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >1</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,428.40 L393.99,428.40 M573.79,428.40 L584.99,428.40 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,428.40 L77.00,428.40 '/> <g transform="translate(53.80,433.60)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >1.5</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,409.10 L393.99,409.10 M573.79,409.10 L584.99,409.10 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,409.10 L77.00,409.10 '/> <g transform="translate(53.80,414.30)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >2</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,389.81 L393.99,389.81 M573.79,389.81 L584.99,389.81 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,389.81 L77.00,389.81 '/> <g transform="translate(53.80,395.01)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >2.5</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,370.51 L584.99,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,370.51 L77.00,370.51 '/> <g transform="translate(53.80,375.71)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="end">
+ <text><tspan font-family="Times" >3</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M65.00,524.88 L65.00,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,524.88 L65.00,512.88 M65.00,370.51 L65.00,382.51 '/> <g transform="translate(65.00,554.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >0</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M195.00,524.88 L195.00,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M195.00,524.88 L195.00,512.88 M195.00,370.51 L195.00,382.51 '/> <g transform="translate(195.00,554.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >5</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M325.00,524.88 L325.00,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M325.00,524.88 L325.00,512.88 M325.00,370.51 L325.00,382.51 '/> <g transform="translate(325.00,554.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >10</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M454.99,524.88 L454.99,436.51 M454.99,382.51 L454.99,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M454.99,524.88 L454.99,512.88 M454.99,370.51 L454.99,382.51 '/> <g transform="translate(454.99,554.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >15</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="gray" stroke="currentColor" stroke-width="0.50" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='gray' stroke-dasharray='2,4' class="gridline" d='M584.99,524.88 L584.99,370.51 '/></g>
+<g fill="none" color="gray" stroke="gray" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M584.99,524.88 L584.99,512.88 M584.99,370.51 L584.99,382.51 '/> <g transform="translate(584.99,554.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >20</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M584.99,505.58 L572.99,505.58 '/> <g transform="translate(596.19,510.78)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="start">
+ <text><tspan font-family="Times" > 0.1</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M584.99,466.99 L572.99,466.99 '/> <g transform="translate(596.19,472.19)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="start">
+ <text><tspan font-family="Times" > 0.12</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M584.99,428.40 L572.99,428.40 '/> <g transform="translate(596.19,433.60)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="start">
+ <text><tspan font-family="Times" > 0.14</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M584.99,389.81 L572.99,389.81 '/> <g transform="translate(596.19,395.01)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="start">
+ <text><tspan font-family="Times" > 0.16</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,370.51 L65.00,524.88 L584.99,524.88 L584.99,370.51 L65.00,370.51 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(16.20,447.70) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >twist angle [deg]</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(646.99,447.70) rotate(270)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >thickness ratio t/c</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(324.99,590.08)" stroke="none" fill="black" font-family="Times" font-size="16.00" text-anchor="middle">
+ <text><tspan font-family="Times" >y [m]</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb( 0, 0, 0)' d='M393.99,436.51 L393.99,382.51 L573.79,382.51 L573.79,436.51 L393.99,436.51 Z '/></g>
+ <g id="gnuplot_plot_1b" ><title>Wing Twist</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(536.62,399.91)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Wing Twist</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb(112, 128, 144)' stroke-dasharray=' 9,4,1,4,1,4' d='M545.01,396.01 L565.40,396.01 M65.00,486.29 L200.18,486.29 L515.60,486.29 '/> <use xlink:href='#gpPt0' transform='translate(65.00,486.29) scale(4.50)' color='rgb(112, 128, 144)'/>
+ <use xlink:href='#gpPt0' transform='translate(200.18,486.29) scale(4.50)' color='rgb(112, 128, 144)'/>
+ <use xlink:href='#gpPt0' transform='translate(515.60,486.29) scale(4.50)' color='rgb(112, 128, 144)'/>
+ <use xlink:href='#gpPt0' transform='translate(555.20,396.01) scale(4.50)' color='rgb(112, 128, 144)'/>
+</g>
+ </g>
+ <g id="gnuplot_plot_2b" ><title>Thickness Distribution</title>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <g transform="translate(536.62,426.91)" stroke="none" fill="black" font-family="Times" font-size="12.00" text-anchor="end">
+ <text><tspan font-family="Times" >Thickness Distribution</tspan></text>
+ </g>
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='rgb( 82, 139, 139)' stroke-dasharray='2.0,5.0,20.0,10.0' d='M545.01,423.01 L565.40,423.01 M65.00,409.08 L200.18,467.09 L515.60,486.38 '/> <use xlink:href='#gpPt1' transform='translate(65.00,409.08) scale(4.50)' color='rgb( 82, 139, 139)'/>
+ <use xlink:href='#gpPt1' transform='translate(200.18,467.09) scale(4.50)' color='rgb( 82, 139, 139)'/>
+ <use xlink:href='#gpPt1' transform='translate(515.60,486.38) scale(4.50)' color='rgb( 82, 139, 139)'/>
+ <use xlink:href='#gpPt1' transform='translate(555.20,423.01) scale(4.50)' color='rgb( 82, 139, 139)'/>
+</g>
+ </g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="2.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="black" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+ <path stroke='black' d='M65.00,370.51 L65.00,524.88 L584.99,524.88 L584.99,370.51 L65.00,370.51 Z '/></g>
+<g fill="none" color="black" stroke="currentColor" stroke-width="1.00" stroke-linecap="butt" stroke-linejoin="miter">
+</g>
+</g>
+</svg>
+
diff --git a/docs/assets/images/screenshots/cmake-gui.png b/docs/assets/images/screenshots/cmake-gui.png
new file mode 100644
index 0000000000000000000000000000000000000000..5ab6cb0a45203bfcd336e3d28e1987d7f8b96809
--- /dev/null
+++ b/docs/assets/images/screenshots/cmake-gui.png
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:212a282280ddf11616e720c08a4fe4ec9a40eb24c691f552dd23ac6125ec9070
+size 49802
diff --git a/docs/assets/images/screenshots/rce.png b/docs/assets/images/screenshots/rce.png
new file mode 100644
index 0000000000000000000000000000000000000000..5454ae024f17536b18c0254398bc1ce6f84c3c44
--- /dev/null
+++ b/docs/assets/images/screenshots/rce.png
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:234426d60a94f95f98e2180b515b793b59744c13616bbce85105beec24b75be8
+size 172536
diff --git a/docs/assets/images/screenshots/tigl.png b/docs/assets/images/screenshots/tigl.png
new file mode 100644
index 0000000000000000000000000000000000000000..c968f4215badeadf1489d30a90d516629f70f76e
--- /dev/null
+++ b/docs/assets/images/screenshots/tigl.png
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:377ad5b9274486aa4ee833c9c6f3c22974cd7c356e937bd27922bf2c9c31f599
+size 209966
diff --git a/docs/assets/javascripts/katex.js b/docs/assets/javascripts/katex.js
new file mode 100644
index 0000000000000000000000000000000000000000..8c642137489081579950e765655a96cd18d93374
--- /dev/null
+++ b/docs/assets/javascripts/katex.js
@@ -0,0 +1,10 @@
+document$.subscribe(({ body }) => {
+ renderMathInElement(body, {
+ delimiters: [
+ { left: "$$", right: "$$", display: true },
+ { left: "$", right: "$", display: false },
+ { left: "\\(", right: "\\)", display: false },
+ { left: "\\[", right: "\\]", display: true }
+ ],
+ })
+})
diff --git a/docs/contact.md b/docs/contact.md
new file mode 100644
index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/description.md b/docs/description.md
index 53be73ed1ff0a8ebd85e91e3867cfa6bb8d4cd04..e4d9ad0b5cdfdb399b3f441dd45baa98dec24fff 100644
--- a/docs/description.md
+++ b/docs/description.md
@@ -1,6 +1,11 @@
## General Description
The general overview of the UNICADO process chain is shown below.
-
+<figure markdown>
+ {width="500"}
+ <figcaption>Overview UNICADO Process</figcaption>
+</figure>
+
+
## Module Descriptions
@@ -10,49 +15,9 @@ the modules of the predecessor MICADO are controlled by the *convergenceLoop* pr
whereas the workflow of UNICADO is programmed in **RCE** (remote control
environment by DLR).
-### Setup Steps
-- [Inital Sizing]()
-- [Fuselage Design]()
-
-### Sizing Loop
-- [createMissionXML]()
-- [wingDesign]()
-- [empennageSizing]()
-- [engineSizing]()
-- [propulsionIntegration]()
-- [calculatePolar]()
-- [massEstimation]()
-- [landingGearDesign]()
-- [systemsDesign]()
-- [missionAnalysis]()
-
-### Post Processing Steps
-
-- Calculate Performance
-- Calculate Costs
-- [DOC Estimation]()
-- [Calculate Emissions]()
-- Report Generator
-- Create Aircraft Stepfile
-- [CPACS Interface]()
-- Design Evaluator
-
-### Additional Software
-
-- parameterStudyMgr
-- [Test Framework]()
-
-### Libraries
-
-- [General on libraries]()
-- [aixml]()
-- [propulsion System]()
-- [Blackbox Tests]()
-- unicadoRuntimeLibs
+!!! note
+ You can refer to the [Module Overview](modules/overview.md) for a list of all available modules.
-Other used libs: aerodynamics, aircraftGeometry, aircraftNetwork,
-atmosphere, engine, liftingLineInterface, runtimeInfo, spline, sqlite3,
-standardFiles, svgPlot, svl, TNT, unitConversion
## Training videos
> :construction: *tbd:* Add link
diff --git a/docs/developer/build-cpp.md b/docs/developer/build-cpp.md
new file mode 100644
index 0000000000000000000000000000000000000000..dd3ba20c4ed4a90ca7dc4307d0c263cc2e08886f
--- /dev/null
+++ b/docs/developer/build-cpp.md
@@ -0,0 +1,199 @@
+---
+title: Building C++ Modules
+summary: How to build C++ modules of UNICADO.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-12
+---
+**UNICADO** uses [CMake :octicons-link-external-16:](https://cmake.org/) for generating the build files.
+CMake is a build system generator, which allows for cross-platform compilation.
+For more information about this system, please refer to its [Documentation :octicons-link-external-16:](https://cmake.org/cmake/help/latest/).
+
+## Configure CMake
+Since **CMake** is independent of the used platform, it needs to figure out on which platform you are running your current build. This process is called *Configuration*. During configuration, **CMake** checks on which platform you are and selects the appropriate build system/compiler.
+**CMake** wants to separate the build specific files from the source files. Usually, this is done by providing a separate *build* directory, where all the intermediate files are stored before actually executing the build.
+With this information in mind the configuration steps are:
+
+1. Open a terminal inside the root directory of the *rAircraftDesign* repository.
+2. Create a folder called `build` if it does not exist yet with `mkdir build`.
+
+ !!! note
+ This *build* folder is not part of the repository.
+
+3. Configure **CMake** by explicitly telling it to generate build files for your platform with the option `-G`:
+
+=== "Windows"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "Visual Studio 16 2019" -A x86 -T ClangCL,hosT=x86
+ ```
+
+=== "MinGW"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "MinGW Makefiles"
+ ```
+=== "Unix"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "Unix Makefiles"
+ ```
+
+During this configuration, **CMake** generates a cache file which remembers some parameters which are re-used when you configure **CMake** again.
+This cache files is __not__ automatically deleted/updated, which can lead to some unexpected behavior.
+When this happens, you can tell **CMake** explicitly to refresh this cache by:
+
+=== "Windows"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "Visual Studio 16 2019" -A x86 -T ClangCL,hosT=x86 --fresh
+ ```
+
+=== "MinGW"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "MinGW Makefiles" --fresh
+ ```
+=== "Unix"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "Unix Makefiles" --fresh
+ ```
+
+Alternatively, you can just delete everything inside the build directory before configuring **CMake** again.
+
+The default build configuration of **CMake** is ^^Release^^. The build configuration can be changed, for example to ^^Debug^^, by:
+
+=== "Windows"
+
+ !!! quote
+ :fontawesome-solid-arrow-right: The *Windows* build system is a so-called **multi configuration generator**.
+ This means its build type can be set during build and does not have to be configured.
+
+=== "MinGW"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "MinGW Makefiles" -DCMAKE_BUILD_TYPE:STRING=Debug
+ ```
+=== "Unix"
+
+ ``` { .sh .copy }
+ cmake -B build -S . -G "Unix Makefiles"-DCMAKE_BUILD_TYPE:STRING=Debug
+ ```
+
+### GUI
+**CMake** also comes with a GUI which can be used for the configuration process.
+The GUI looks like this:
+
+
+
+It works the same as the command line interface.
+You have to specify the path to the source files and to the build directory.
+You also see the exposed options of the project.
+And as the GUI already tells you:
+> Press Configure to update and display new values in red, then press Generate to generate selected build files.
+
+### Options
+These project options are currently available during configuration time:
+
+| Name | Default | Description |
+| --- | :---: | ---|
+|**BUILD_BLACKBOXTESTS**| `OFF` | Whether to build the blackbox tests. (If available)|
+|**BUILD_UNITTEST**| `OFF` |Whether to build the unit tests. (If available)|
+|**BUILD_SHARED_LIBS**| `OFF` | Decide whether the libraries are built as static or shared libraries.|
+|**PACKAGE_SYSTEM_LIBRARIES**| `OFF` | Whether to include all system libraries when creating release packages. *(Only available in `rUNICADO`)* |
+|**FIND_LIBRARIES_AS_PACKAGE**| `OFF` |If *true* the libraries are included with `find_package()`, otherwise the *submodule* with `add_subdirectory()` is used.|
+|**STATIC_GLIBS**| `OFF` | Whether to link the *GCC runtime libraries* as static libraries. :warning: ^^**Experimental**^^ |
+
+The other options shown in the GUI are specific to **CMake**.
+(*Not all options shown in the table are part of the screenshot, since the screenshot was taken before these options were introduced.*)
+
+---
+
+## Build with CMake
+**CMake** also provides a convenient interface to invoke the build system without you needing to know which build system is actually used.
+The different modules or executables are called *targets* in the **CMake** language.
+So to build a specific target you call **CMake** with the following command, where `build` is the created build directory and `the-target` is the name of the module you want to compile:
+
+=== "Windows"
+
+ ```sh
+ cmake --build build --target the-target --config build-type
+ ```
+ :fontawesome-solid-arrow-right: The `build-type` can be one of the usual suspects:
+
+ - **Release**
+ - **Debug**
+ - **MinSizeRel**
+
+=== "MinGW"
+
+ ```sh
+ cmake --build build --target the-target
+ ```
+
+ !!! tip
+ Remember: the build type is already specified when configuring **CMake** :point_up:.
+
+=== "Unix"
+
+ ```sh
+ cmake --build build --target the-target
+ ```
+
+ !!! tip
+ Remember: the build type is already specified when configuring **CMake** :point_up:.
+
+When you want to compile all the modules ^^at once^^, you can just omit the *target* option and call **CMake** with:
+
+=== "Windows"
+
+ ```sh
+ cmake --build build --config build-type
+ ```
+
+=== "MinGW"
+
+ ```sh
+ cmake --build build
+ ```
+
+=== "Unix"
+
+ ```sh
+ cmake --build build
+ ```
+
+You can also clean the build before re-compiling:
+
+=== "Windows"
+
+ ```sh
+ cmake --build build --target the-target --config build-type --clean-first
+ ```
+
+=== "MinGW"
+
+ ```sh
+ cmake --build build --target the-target --clean-first
+ ```
+
+=== "Unix"
+
+ ```sh
+ cmake --build build --target the-target --clean-first
+ ```
+
+That's all folks. This should compile *UNICADO* just fine. 👌
+
+!!! warning
+ Make sure to update your **PATH** with the new runtime libraries (when compiled as shared libraries), which are located in: /path-to-libs-submodule/unicadoRuntimeLibs/
+
+### Improve Compilation Speed
+You can increase the build speed by enabling parallel jobs of the build tool. This is as easy as this:
+
+```sh
+cmake --build build --target the-target -j n-jobs
+```
+
+This builds the project using `n-jobs` processes. You can give any number here, but it should correspond to the number of processors available on your machine.
diff --git a/docs/developer/build-python.md b/docs/developer/build-python.md
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diff --git a/docs/developer/contribute.md b/docs/developer/contribute.md
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diff --git a/docs/developer/environment-cpp.md b/docs/developer/environment-cpp.md
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index 0000000000000000000000000000000000000000..50653fd6398181da47047564bd8b7daa045a1171
--- /dev/null
+++ b/docs/developer/environment-cpp.md
@@ -0,0 +1,10 @@
+
+## Build
+
+=== "Unix"
+
+ When using Unix
+
+=== "Windows"
+
+ When using windows
\ No newline at end of file
diff --git a/docs/developer/environment-python.md b/docs/developer/environment-python.md
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index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/developer/ide-setup.md b/docs/developer/ide-setup.md
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index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/developer/including-libraries.md b/docs/developer/including-libraries.md
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index 0000000000000000000000000000000000000000..f4d41a10c301efdc0a6a30aa04636967863f371f
--- /dev/null
+++ b/docs/developer/including-libraries.md
@@ -0,0 +1,56 @@
+---
+title: Build and Include the Libraries
+summary: Some remarks on including the UNICADO libraries.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-12
+---
+## A word about including the libraries
+
+Oh yes, the **UNICADO** [libraries](../modules/libraries.md). 🙂
+When you start developing and building the **UNICADO** modules you will quickly discover the importance of the libraries.
+There are many ways how you can include libraries in C++ projects and all have their advantages and disadvantages.
+In the **UNICADO** project, the most important decisions to make are:
+
+- Whether to include the libraries as **static** (`*.a`) or **dynamic** (`*.dll` or `*.so`) libraries.
+- Whether to include the libraries as **CMake** **targets** and always recompile the libraries when building the modules or to import the libraries as a **CMake** **package** somewhere from the hard drive. ( :fontawesome-solid-arrow-right: Look in [ Include Library Package ](#) to find out what this actually means.)
+
+
+> Note that each decision is completely independent from the other decision.
+
+Each of those decisions has a corresponding option when configuring **CMake**.
+So you can decide for your situation what suits your workflow the best.
+The default configuration when [Building with CMake](build-cpp.md) is:
+
+- `BUILD_SHARED_LIBS=OFF` :fontawesome-solid-arrow-right: Build **static** libraries.
+- `FIND_LIBRARIES_AS_PACKAGE=OFF` :fontawesome-solid-arrow-right: Include **targets** from the submodule and recompile libraries each time there are changes.
+
+!!! note
+ The default configuration is usually best suited for most situations.
+
+## Changing to dynamic libraries
+When you want to decrease the binary size of the executables or want to test changes in the libraries without having to recompile the executables, you can build the libraries as **dynamic** libraries by configuring **CMake** with:
+
+```sh
+cmake -B build -S . -G "your-generator" -DBUILD_SHARED_LIBS=ON
+```
+
+This will build all libraries as **dynamic** libraries and link the executables against those libraries.
+It does not matter where you set this option.
+When you build the libraries on their own, the option does the same thing as when you build the complete project where the libraries are included as a submodule.
+
+!!! warning
+ Do not forget to add the location of the **dynamic** libraries to your **PATH** afterwards. 😉
+
+## Changing to the library package
+
+When you want to save some compilation time or do not want to copy the libraries everywhere, you can include them as a package by:
+
+```sh
+cmake -B build -S . -G "your-generator" -DFIND_LIBRARIES_AS_PACKAGE=ON -DCMAKE_PREFIX_PATH=path-to-libs
+```
+
+!!! important
+ When including the libraries as a package you ^^**HAVE**^^ to set `CMAKE_PREFIX_PATH` as described in [ Include Library Package ](#). You also have to make sure that the libraries this path is pointing to are compiled and exist!
+
+With this mechanism you can have mutliple projects using the same libraries without having to copy and recompile them all the time. The added downside is that **CMake** can no longer handle the automatic compilation and you have to manually make sure that the libraries are ready to be used.
\ No newline at end of file
diff --git a/docs/developer/prerequisites.md b/docs/developer/prerequisites.md
new file mode 100644
index 0000000000000000000000000000000000000000..1b32b9779958b4c22d083621b313d4db69bee557
--- /dev/null
+++ b/docs/developer/prerequisites.md
@@ -0,0 +1,9 @@
+---
+title: Build Instructions
+summary: Contains the instruction to get the build process up and running.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-06
+glightbox: false
+---
+# Build Instructions
\ No newline at end of file
diff --git a/docs/developer/setup.md b/docs/developer/setup.md
new file mode 100644
index 0000000000000000000000000000000000000000..958f7d5f0f7fb51174ed9f13c7f0d891d9b2ec39
--- /dev/null
+++ b/docs/developer/setup.md
@@ -0,0 +1,8 @@
+---
+title: Software Development Setup
+summary: How to setup the environment to successfully contribute to UNICADO.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-06
+glightbox: false
+---
diff --git a/docs/developer/style/cpp.md b/docs/developer/style/cpp.md
new file mode 100644
index 0000000000000000000000000000000000000000..478b28130ab28ae7a31801c4185aee496d5db71e
--- /dev/null
+++ b/docs/developer/style/cpp.md
@@ -0,0 +1,239 @@
+---
+title: C++ Style Guide
+summary: The most important C++ style rules for UNICADO.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-12
+---
+# UNCIADO C++ Style Guide
+
+!!! tip
+ Consistency in code style is the most important thing!
+
+---
+
+## Standard Module Design
+- Calculations not in `aircraft.cpp` (aircraft is pure data object)
+- `myTool.cpp` for calculations, has (smart) pointers to Aircraft and Settings objects
+- Do not edit standard files like aircraft.cpp, functions.cpp etc. ->use own files (myToolFunctions, myToolspecificAicraftData,...)
+
+### Structure main()
+1. Create Settings object
+2. Create aircraft object
+3. Create myTool-object, if necessary call init()
+4. Call myTool.run()
+5. Create output and call writeOutput()
+6. Done
+
+!!! warning
+ :fontawesome-solid-arrow-right: The module structure changed in newer releases of **UNICADO**. See [Module Structure]().
+
+---
+
+## Header Files
+### Inline Functions
+- Define inline functions only if they are small (~ 10 lines or less).
+
+### Function Parameter Ordering
+- The sequence of parameters of a function is: first input parameters, then output parameters.
+- Input parameters are passed either as value or const reference.
+- Output or input/output parameters are passed as pointers.
+
+:fontawesome-solid-arrow-right: In general, try to use **value semantics** instead of reference/pointer semantics.
+
+---
+
+## Classes
+### Doing Work in Constructors
+- No errors may be thrown in the constructor.
+- Short initialization in the constructor is ok.
+- Transfer complex initialization with larger calculation in initialization method (e.g. `Init()`).
+- Do not call `init()` in the constructor, but after constructor call!
+
+### Inheritance
+- Destructor must always be virtual if it should be a base class for other classes.
+
+### Declaration Order
+- Declaration sequence: public, protected, private. In every section:
+ - Typedefs and Enums
+- Constants (static const data members)
+- Constructors
+- Destructor
+- methods, incl. static methods
+- Data Members (except static const data members)
+- for constants: first const then data type, e.g.: `const int i = 1;`
+
+### Write Short Functions
+- Prefer small and focused functions.
+- For more than 40 lines: split the function
+
+### Ownership and Smart Pointers
+- Always use Smart Pointers instead of normal pointers (raw pointers), since Smart Pointers free up storage space at a suitable location.
+- Do not use `auto_ptr` (obsolete and not container-compatible) but `unique_ptr`.
+- Use `shared_ptr` only if several pointers to the same object are needed, because more memory is used for the reference counting.
+
+---
+
+## Other C++ Features
+### Preincrement and Predecrement
+- For primitive data types, post-increment `i++` is the same as pre-increment `++i`.
+- Pre-increment is faster for iterators because no copy is created.
+- For iterators: use pre-increment
+
+### auto
+- Only use `auto` when the type is still clear to the reader.
+- Example:
+
+```cpp
+/* static_cast holds the type clearly visible */
+auto value = std::static_cast<int>(other_value);
+```
+- Use `auto` for **trailing return types** of functions, because we are doing **Modern C++** 😉 :
+
+```cpp
+auto some_function(int input) -> double
+{
+ /* do stuff */
+ return value;
+}
+```
+- Do __not__ use `auto` when the type is not clearly visible.
+- Don't:
+
+```cpp
+auto value = get_value(); // type ist not readable
+```
+
+### Comparison of variables of type double
+- In order to avoid a compiler warning if floating values are compared (== or !=) use the function `fabs(a-b) < ACCURACY_LOW / _MEDIUM / _HIGH`. **LOW**, **MEDIUM** and **HIGH** correspond to accuracies of **10e-4**, **10e-7** and **10e-10**, respectively. Choose the accuracy as necessary for each case. Alternatively, you can also use the function `accuracyCheck(a, b, ACCURACY_LOW / _MEDIUM / _HIGH)`.
+- Accuracy constants can be found in the :fontawesome-solid-file: `constants.h` file within the unitConversion library.
+
+---
+
+## Naming
+- Function names, variable names and file names should be descriptive: no simple letters such as "b" for span.
+- Avoid abbreviations: Don't delete letters from words in the name to make it shorter e.g.: acft_dsgn instead of aircraft_design (usual and common abbreviations are fine in case of doubt)
+- Lowercase file names, variable names and function names; capitalize new word
+- Capitalize Structs, Typdefs and Enums
+- Names should be as short as possible, but as long as necessary
+
+---
+
+## Comments
+- The best code is self-explaining --> good type & variable names, etc.
+- Documentation with Doxyblocks; see also "Documentation with Doxyblocks.pptx".
+- You can use `\` and `@` to mark the __doxygen__ keywords.
+- Generally everywhere, where the code is not directly understandable by itself, comments on readability and comprehensibility are necessary.
+- But don't describe the code itself. Assume that the reading person knows C++.
+- Do not use umlauts (ä -> ae etc.)
+
+### File Comments
+- Line comments for attributes in header: Declaration `/**<Comment*//`
+- Each file should have a comment at the beginning describing its contents.
+- Header file `.h`: Describes the classes declared in the file. [icon arrow-right} what are they for, how are they used?
+- Source file `.cpp`: Contains more information about implementation details / algorithms.
+- Implementation details and information about algorithms can also be mentioned in.h file, but then mention in `.cpp` file Location of documentation.
+- The files should always start with a copyright statement.
+- After the copyright, give some information about the file with:
+
+```cpp
+/**
+ * \file name.extension
+ * \author Name (Email)
+ * \brief Short description of the content
+ * \version major.minor.bugfix
+ * \date yyyy-mm-dd
+ */
+```
+
+### Class Comments
+- Each class should have an accompanying comment describing what the class is for and how it is used
+- Block comments for classes in source:
+
+```cpp
+/**
+ * \class name
+ * \brief short description of the class
+ * \details detailed description of the class
+ */
+```
+
+### Function Comments
+- Function declaration: Describe what the function does and how it is used.
+- Does the memory function occupy memory that must be released again by the caller?
+- Can one of the arguments be a null pointer?
+- Definition of function: Describe how the function performs its task.
+- Give an overview of the individual steps.
+- Explain the used "coding tricks".
+- Explain why this implementation was chosen.
+- Block comments for methods/constructors in Source:
+
+```cpp
+/**
+ * \brief description of the function/method/constructor
+ * \details detailed description of the method
+ * \param name Description of the transfer parameter
+ * \return name Description of the return value
+ */
+```
+
+- Additional comments in the code only via `//`.
+- Instructions for creating documentation with Doxyblocks can be found in the wiki.
+
+### TODO Comments
+- Use **TODO** comments to mark temporary code, temporary solutions or parts in need of improvement.
+- Example for formatting: `// TODO(Name#_#MantisID:_) Comment`
+- A **TODO** is not an obligation that the specified person will solve the problem.
+- Specify an approximately date/time frame, if necessary, in which the problem is to be solved.
+
+---
+
+## Formatting
+- General (ANSI) style with 4 spaces as indentation.
+
+### Line Length
+- Each line of code max. 120 characters’ long.
+- Exception: Comment line with example or URL.
+
+### Spaces vs. Tabs
+- Use only spaces, 4 spaces for an indentation.
+- IDE can be set to output spaces at "TAB".
+
+:fontawesome-solid-arrow-right: For a more detailed description of settings see Wiki article on [Linter Setup]().
+
+== Function Declarations and Definitions ==
+- Return type and function name in one line.
+- Parameter in the same line if it does not match: Parameters in several lines
+- No space between function name and opening parenthesis.
+- No space between parenthesis and parameter.
+- Example:
+
+```cpp
+auto ClassName::functionName(Type par_name1, Type par_name2) -> return_type
+{
+ DoSomething(); // 2 space indent
+}
+```
+
+### Horizontal Whitespace
+- No spaces at end of line.
+- For operators (=, <, >, +, -, ...): space before and after: `int a = 0;` (not `int a=0;`)
+- Sometimes spaces can be removed by factors: `v = w*x + y/z;`
+- In loops and conditions: Spaces before the beginning of parentheses and after semicolons; no additional spaces in parentheses.
+- Can be automated in the IDE under the button Source "Formatter Insert Spaces around operators".
+
+### Vertical Whitespace
+- Minimize empty lines!
+- Basic rule: The more code fits on the screen, the easier it is to follow the program flow.
+- Blank lines at the beginning and end of functions can sometimes improve readability.
+
+!!! tip
+ This code style is based on the Google C++ Style Guide [GSG :octicons-link-external-16:](https://google.github.io/styleguide/cppguide.html) and contains some guidelines. For more information or more detailed specifications, read the Google Guide.
+
+---
+
+## Bibliography
+
+**GSG**: Google, [Google C++ Style Guide :octicons-link-external-16:](https://google.github.io/styleguide/cppguide.html)
+
+**ISOCPP**: IsoCpp, Bjarne Stroustrop & Herb Sutter, [C++ Core Guidelines :octicons-link-external-16:](http://isocpp.github.io/CppCoreGuidelines/CppCoreGuidelines)
diff --git a/docs/developer/style/python.md b/docs/developer/style/python.md
new file mode 100644
index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/installation.md b/docs/getting-started/installation.md
similarity index 100%
rename from docs/installation.md
rename to docs/getting-started/installation.md
diff --git a/docs/getting-started/takeoff.md b/docs/getting-started/takeoff.md
new file mode 100644
index 0000000000000000000000000000000000000000..4b8b8b2aa9d8bca166904a9f64bd1ae86b7fa61c
--- /dev/null
+++ b/docs/getting-started/takeoff.md
@@ -0,0 +1,83 @@
+---
+title: Cleared for Take-Off
+summary: Instructions how to run the workflow
+authors:
+ - Sebastian Oberschwendtner
+ - Maurice Zimmnau
+date: 2023-09-08
+---
+## UNICADO Workflow
+
+For the full experience of aircraft design, start RCE and run the workflow
+Download and install the workflow with the current [UNICADOinstaller]().
+
+---
+
+## Separate tool execution
+
+You may want to build and execute UNICADO tools separately. Here we go:
+
+### Requirements
+
+Clone the following repositories:
+
+- **rAIRCRAFTDESIGN** - aircraft design tools
+- **rAIRCRAFTREFERENCES** - aircraft reference designs
+- **rADDITIONALSOFTWARE** - additional not aircraft design specific tools, e.g. for plotting
+
+NOTE: the repositories **rAIRCRAFTDESIGN** and **rADDITIONALSOFTWARE** shall be checked out on the same branch (e.g. *develop*), as those branches are synchronized on remote ☁ and a running 🏃 🏃 couple 💍
+
+For testing purposes you most probably will choose the CSR-02 aircraft reference. Therefore, checkout the *CSR-02* branch from the **rAIRCRAFTREFERENCES** repo.
+
+---
+
+### Project Environment
+
+For creating a {nav project environment} you have several options 🍟. Here we'll present the two mostly used ones (Excluding the UNICADOworkflow on RCE stated at top)
+
+- Create a new folder for your project environment **or** use the folder where you have cloned the **rAIRCRAFTDESIGN** repo
+- Copy {nav Gnuplot} and {nav Inkscape} from the folder where you have cloned the **rADDITIONALSOFTWARE** repo into your {nav project environment}
+{nav name=project environment > Gnuplot }
+{nav name=project environment > Inkscape }
+NOTE: If you are using a unix based system make sure to copy the linux variants of *Gnuplot* and *Inkscape* named *Gnuplot-linux* and *Inkscape-linux*
+
+- Copy the tool(s) you want to execute / test (e.g. *initialSizing*) from your local copy of **rAIRCRAFTDESIGN** (In case you are **not** using the local copy itself as a **project environment**)
+{nav name=project environment > initialSizing }
+- Create a folder named *projects* within your **project environment**
+{nav name=project environment > projects }
+- Within your *projects* folder create a folder named as the aircraft class, e.g. {nav CSR} (CeRAS Short Range)
+{nav name=project environment > projects > CSR }
+- Within the aircraft class folder create a folder of the aircraft type, e.g. {nav CSR-02}
+{nav name=project environment > projects > CSR > CSR-02 }
+- Copy the **content** (not the folder) of a specific design folder of the corresponding aircraft from your local copy of **rAIRCRAFTREFERENCES** into the aircraft type folder. Options are
+{nav cleanSheetDesign}
+{nav retrofitDesign > aerodynamicCalibration}
+{nav retrofitDesign > engineCalibration}
+{nav retrofitDesign > withoutCalibration}
+- Now you have again two options: **1.** Test the tool on an empty aircraft exchange file. **2.** Test the tool on a so called converged aircraft.
+ - For **1.** Delete the existing aircraft exchange fiel e.g. *CSR-02.xml*. Then rename the aircraft exchange file e.g. *CSR-02_startCSD.xml* to *CSR-02.xml* (if you have copied the cleanSheetDesign [CSD])
+ - For **2.** Directly execute your tool with the available aircraft exchange file, e.g. *CSR-02.xml*
+
+
+---
+
+### Aircraft Design Tool Dependencies
+
+Suppose you use an empty aircraft exchange file (described above in option **1.**).
+The aircraft design tools have dependencies, e.g. a fuselage 🐳 has to exist in order to mount wings 🐦. An aircraft geometry has to be available in order to conduct an aerodynamic analysis.
+
+Therefore the tools can be executed based on their dependencies in the following sequence:
+{nav initialSizing > fuselageDesign > createMissionXml > wingDesign > empennageSizing > engineSizing > propulsionIntegration > landingGearDesign > calculatePolar > massEstimation > systemsDesign > missionAnalysis}
+
+---
+
+### Tool execution
+
+Finally we want to execute the tool. But what if we have noticed, that there are no executables in the tool folders? 🔥
+Then the executables have first to be build inside the working copy e.g. of the **rAIRCRAFTDESIGN** repo. Please follow the instructions at [[ software_development_setup/ ]] and [[ build_instructions/ ]]
+
+If this is done already and an executable is present, then you can execute the respective tool from within the tool folder either on windows directly via double click or via a terminal
+- In cmd or powershell e.g. `initialSizing.exe`
+- In git bash e.g. `./initialSizing.exe`
+
+If you want to examine the terminal outputs we've got you covered: `.log`-files are written for each tool
diff --git a/docs/impressum.md b/docs/impressum.md
new file mode 100644
index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/index.md b/docs/index.md
index fe80567a4126a0afd22e840dc4665ac8c6ce5f47..8991514bcb7839d5640159000514d2a1b5d14fdc 100644
--- a/docs/index.md
+++ b/docs/index.md
@@ -1,3 +1,62 @@
+---
+title: Welcome to UNICADO
+summary: Home page of the UNICADO project
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+
+
# Welcome to UNICADO
+**UNICADO** is a preliminary aircraft design tools which groups many design modules.
+Go through the following stuff to get an idea what **UNICADO** is and how it works:
+
+<div class="grid-container" markdown="1">
+<div class="grid-item" markdown="1">
+
+:material-clock-fast:{ .lg .middle } **Getting Started**
+
+---
+
+Learn how to set it up and install the required prerequisites.
+
+[:octicons-arrow-right-24: Getting Started](getting-started/installation.md)
+
+</div>
+<div class="grid-item" markdown="1">
+
+:fontawesome-solid-plane-departure:{ .lg .middle } **Cleared for Take Off**
+
+---
+
+Start designing aircraft to your requirements.
+
+[:octicons-arrow-right-24: Start Designing](getting-started/takeoff.md)
+
+</div>
+<div class="grid-item" markdown="1">
+
+:material-library:{ .lg .middle } **Available Tools**
+
+---
+
+Get an overview which tools and components are available within **UNICADO**.
+
+[:octicons-arrow-right-24: Module Overview](modules/overview.md)
+
+</div>
+<div class="grid-item" markdown="1">
+
+:material-scale-balance:{ .lg .middle } **Open Source**
+
+---
+
+**UNICADO** is available as open source software licensed under **GPLv3**.
+
+[:octicons-arrow-right-24: License](license.md)
+
+</div>
+</div>
-
+{width="400"}
\ No newline at end of file
diff --git a/docs/license.md b/docs/license.md
new file mode 100644
index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/modules/additional-software.md b/docs/modules/additional-software.md
new file mode 100644
index 0000000000000000000000000000000000000000..340b7a9df547d90c6f9b5102641afa9816776d62
--- /dev/null
+++ b/docs/modules/additional-software.md
@@ -0,0 +1,56 @@
+---
+title: Additional Software
+summary: Overview of the additionalSoftware repository
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+
+## cpacsInterface
+{.overview-img align=left}
+The **cpacsInterface** is an additional module of the UNICADO toolchain.
+Its purpose is to transform the UNICADO aircraft XML file into CPACS format and vice Versa.
+The module consists of two modules convertUNICADO2CPACS which is responsible for converting the UNICADO aircraft exchange file into a CPACS format document, and convertCPACS2UNICADO which does the exact opposite and convert the data of the CPACS file into UNICADO format file.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## designEvaluator
+{.overview-img align=left}
+The **deignEvaluator** can be used to perform all available analysis on a designed aircraft and create all available reports for it.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## reportGenerator
+{.overview-img align=left}
+The program collects all :simple-latex: reports of the programs and compiles a total pdf-report.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## testFramework
+{.overview-img align=left}
+The **testFramework** is the heart of the **UNICADO** test pipeline.
+It can perform all required test at the different hierarchy levels.
+It is mainly an automation tool written specifically for the **UNICADO** project.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-python: |GPLv3|[Link]()|
+
+---
diff --git a/docs/modules/analysis.md b/docs/modules/analysis.md
new file mode 100644
index 0000000000000000000000000000000000000000..7b9bed3c4a963f377a74271a2c03f2368c44094f
--- /dev/null
+++ b/docs/modules/analysis.md
@@ -0,0 +1,98 @@
+---
+title: Analysis
+summary: Overview of the analysis modules of aircraftDesign repository
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+# Analysis Tools
+
+---
+
+## calculateEmissions
+{.overview-img align=left}
+The **calculateEmissions** is an additional module of the UNICADO toolchain.
+Its purpose is to calculate the emissions and energy demand within the aircraft's lifecycle and to determine the missions based climate impact.
+For the user, possible changes in the module run configuration can be made in the related calculateEmissions_conf.xml file.
+The parameters comprised in this XML file can have different attributes as e.g. Filenames, Directories, Output configs, and are further subdivided into control and program settings.
+{.overview-item}
+
+!!! note
+ By now, only the calculation routines / outputs based on the flown mission are up to date.
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## calculatePerformance
+{.overview-img align=left}
+The module `calculatePerformance` is used to evaluate the mission performance of the design.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus:| GPLv3 |[Link]()|
+
+---
+
+## calculatePolar
+{.overview-img align=left}
+The tool `calculatePolar` calculates, as the tool name suggests, the polars of an aircraft.
+CalculatePolar uses the tool Lifting Line from DLR to calculate force, lift and moment coefficients for each lifting surface of the aircraft.
+These coefficients are used to calculate induced, viscous and wave drag as well as the moment coefficients for the overall aircraft.
+Furthermore polars are not only calculated for off-design mach numbers but also for high
+lift mach numbers.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## costEstimation
+{.overview-img align=left}
+This modules calculates the direct operating cost (DOC) of an aircraft.
+Direct costs include all expenses incurred in operating and financing the aircraft:
+
+- Fuel
+- Crew
+- Maintenance
+- Fees
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-python: |GPLv3|[Link]()|
+
+---
+
+## massEstimation
+{.overview-img align=left}
+The Mass Estimation module calculates sub-masses and total masses of the aircraft including center of gravities.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## missionAnalysis
+{.overview-img align=left}
+The module `missionAnalysis` is the key module of the aircraft performance analysis.
+Its purpose is to calculate the flight trajectory, based on the inputs of the preliminary aircraft design cycle, by solving the aircraft equations of motion being simplified as a point mass model.
+Depending on the method, the fuel consumption is calculated either:
+
+- in segments by using the Breguet range formula, or
+- in a full-mission time-history simulation (the flight mission is divided into increments. For each increment the movement equations are solved, followed by the thrust requirements and fuel consumption)
+
+For the user, possible changes in the module run configuration can be made in the related *missionAnalysis_conf.xml* file. The parameters comprised in this XML file can have different attributes as e.g. Desc, Unit, Default, AllowedRelOvershoot or text and are further subdivided into control and program settings.
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
\ No newline at end of file
diff --git a/docs/modules/libraries.md b/docs/modules/libraries.md
new file mode 100644
index 0000000000000000000000000000000000000000..c5a8d6642d29e5fe5519687755f67df919182a50
--- /dev/null
+++ b/docs/modules/libraries.md
@@ -0,0 +1,205 @@
+---
+title: Libraries
+summary: Overview of the libraries respository
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+
+## aerodynamics
+{.overview-img align=left}
+This library helps with interacting with polar data.
+It has helper functions to extract and interpolate data of provided airfoil polars.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## aircraftGeometry
+{.overview-img align=left}
+This library defines geometry classes which are generally used within an aircraft.
+The geometry describes the general shape of the different components.
+The available components are:
+
+- *liftingSurface*
+- *verticalSurface*
+- *Fuselage*
+- *Nacelle*
+- *Pylon*
+- *Landing Gear*
+
+The library furthermore provides functions to extract and measure geometry properties of the different shapes at certain locations.
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.0.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## aircraftGeometry2
+{.overview-img align=left}
+This library is based on the older [aircraftGeometry](#aircraftgeometry) library and extends it to be more modular.
+The modularity and flexibility is achieved by using the high performance [Computational Geometry Algorithms Library](https://www.cgal.org/) also known as **CGAL**.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link](aircraftGeometry2/index.html)|
+
+---
+
+## aircraftNetwork
+{.overview-img align=left}
+This library can be used to define wiring harnesses within an existing aircraft geometry.
+You can route wire through different points and analyse the resulting network.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## aixml
+{.overview-img align=left}
+The **aixml** library is the central library which handles the XML files and data access.
+It uses a simple XML library, namely *tinyxml*, to read and parse the XML files.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## atmosphere
+{.overview-img align=left}
+The **atmosphere** library provides helper functions to calculate atmospheric properties according to the International Standard Atmosphere (*ISA*).
+You can set different atmospheric conditions (e.g. *ISA+25*) and calculate the physical properties of the air at different altitudes.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## engine
+{.overview-img align=left}
+This library helps with interacting with engine data.
+It has helper functions to extract and interpolate data of provided engine data decks.
+The engine decks can originate from different softwaretools as long as they provide the same file format.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## liftingLineInterface
+{.overview-img align=left}
+This library helps with interacting with results provided by the tools **Lifting Line** from DLR.
+It has helper functions to extract and interpolate data of the results from the tool.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## moduleBasics
+{.overview-img align=left}
+This library provides the basis structure for the modular approach of the **UNCIADO** tools.
+The tools are intended to follow the *Strategy Design Pattern* to execute at different fidelity levels.
+The library gives a template how modules should be structured and gives helpers which can be used to select and implement the different fidelity methods.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## propulsionsystem
+{.overview-img align=left}
+This is a versatile tool which can be used to simulate and analyse the power flow within an aircraft.
+The power flow is mainly determined by the propulsive systems onboard, but the tool can account for other power needed during operation as well.
+The propulsion systems are not limited to conventional types.
+Due to the flexible abstraction via so-called *two-terminal block*, any system which as inputs and outputs can be implemented.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+!!! info
+ Since this is a standalone tool it will most likely move to another repository in the next release.
+
+---
+
+## runtimeInfo
+{.overview-img align=left}
+This library handles the user interface during the modules execution.
+In provides custom output streams, which automatically handle the log files and error outputs according to the configuration files.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## spline
+{.overview-img align=left}
+The name gives it away: this library provides spline functionality for interpolating data or geometry.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## standardFiles
+{.overview-img align=left}
+This library provides file interfaces and interacts with the operating system.
+It can handle process execution with a simple interface.
+The library can handle *UNIX* and *Windows* systems alike.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+!!! warning
+ Some functions of this library are a bit outdated! When using this library, please look first at the wonderful [STL :octicons-link-external-16:](https://en.cppreference.com/w/) whether the function you are seeking is already there.
+
+---
+
+## svgPlot
+{.overview-img align=left}
+This library interact with the shapes defined by [aircraftGeometry](#aircraftgeometry) and can create different views of the shapes in **SVG** format.
+You can insert text and measurements for quickly creating meaningful reports.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## unitConversion
+{.overview-img align=left}
+The **unitConversion** groups the most commonly used unit in aerospace and let's you convert values from one unit to another.
+In addition, it defines some common **constants** which are useful for calculations.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
\ No newline at end of file
diff --git a/docs/modules/overview.md b/docs/modules/overview.md
new file mode 100644
index 0000000000000000000000000000000000000000..0aa003a8b81fe457e1a5ed511a251c9b25794e8a
--- /dev/null
+++ b/docs/modules/overview.md
@@ -0,0 +1,41 @@
+---
+title: Overview
+summary: Overview of the software groups.
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+
+**UNICADO** collects several modules and data which are grouped into repostories:
+
+- [:simple-gitlab: Aircraft Design :octicons-link-external-16:]():
+
+ The aircraft design repository collect alls the [sizing tools](sizing.md) and [analysis tools](analysis.md) which are needed for the preliminary design process.
+
+- [:simple-gitlab: Libraries :octicons-link-external-16:]():
+
+ Whenever some functionality is used in several modules, the functions are collected and made available within the project via [libraries](libraries.md).
+
+- [:simple-gitlab: Additional Software :octicons-link-external-16:]():
+
+ Tools which are not directly needed for the aircraft design process, like our test framework are grouped in [additional software](additional-software.md). Some helper tools which are used to convert file types and analyse results can be found here as well.
+
+- [:simple-gitlab: Aircraft References :octicons-link-external-16:]():
+
+ Here you can found different designed aircraft. The designs are made using the **UNICADO** workflow and are generally in a *valid* and *converged* state.
+
+!!! note
+ This repository will be translated to a actual database in the future!
+
+- [:simple-gitlab: Engines :octicons-link-external-16:]():
+
+ This collect different engines and their operating data as lookup tables which is used by several tools to analyse and estimate the engine performance.
+
+- [:simple-gitlab: WorkflowOnRCE :octicons-link-external-16:]():
+
+ Here are all the files which are relevant for executing the **UNICADO** workflow with [RCE]().
+
+- [:simple-gitlab: UNICADO :octicons-link-external-16:]():
+
+ This repository is a container which collects all **UNICADO** repositories as submodules. It is used to create the **UNICADO** releases and is a **good** starting point to get developing.
\ No newline at end of file
diff --git a/docs/modules/sizing.md b/docs/modules/sizing.md
new file mode 100644
index 0000000000000000000000000000000000000000..dc1c33786bd38d590d218e3284c68ea8acc9a07c
--- /dev/null
+++ b/docs/modules/sizing.md
@@ -0,0 +1,140 @@
+---
+title: Sizing
+summary: Overview of the sizing modules of aircraftDesign repository
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+glightbox: false
+---
+# Sizing Tools
+The sizing tools design and estimate aircraft parameters.
+They mainly change the dimensions of the aircraft and systems.
+The following sizing tools are available:
+
+---
+
+## createMissionXML
+{.overview-img align=left}
+The **createMissionXML** is the third module of the UNICADO tool chain.
+Its purpose is to set up the overall flight mission including e.g. a flight segment table, speed and altitude schedules, number of passengers (PAX), total payload or the engine warm up time.
+For the user, possible changes in the module run configuration can be made in the related createMissionXML_conf.xml file.
+The parameters comprised in this file can have different attributes as e.g. Desc, Unit, Default or #text and are further subdivided into control settings and program settings.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## empennageSizing
+{.overview-img align=left}
+The **empennageSizing** module calculates characteristic parameter of the empennage of the aircraft.
+It takes takes the controllability as wells as the static margin of the aircraft into account and sizes the empennage accordingly.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## engineSizing
+{.overview-img align=left}
+Currently one engine performance deck is available (of the V2527-A5 engine).
+This performance deck was created with an external calculation tool.
+The engine performance deck containing serval parameters (like thrust, fuel-flow, ...) as a function of the flight Mach number and the altitude.
+This deck is the basis for the UNICADO engineSizing module.
+The engine will be scaled by the engineSizing module to match the specific thrust requirements.
+Moreover, an engine bucket curve and several engine deck plots can be created.
+Also, the engineSizing module set the required parameters of the engine performance for the aircraft design process in the central aircraft exchange file.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## fuselageDesign
+{.overview-img align=left}
+The **fuselageDesign** module calculates characteristic parameters and generates the passenger cabin and fuselage layout for the entire aircraft project.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## hydrogenTank
+{.overview-img align=left}
+:construction: *tbd*
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-python: |GPLv3|[Link]()|
+
+---
+
+## initialSizing
+{.overview-img align=left}
+The module **initialSizing** is used to determine a design chart regarding Top Level Aircraft Requirements and Certification Specification Requirements.
+The wing-loading ($\frac{W}{S}$) and thrust to weight ratio ($\frac{T}{W}$) can be derived as the design point for further modules from the Design Chart.
+Furthermore an initial estimation of the takeoff mass is done.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## landingGearDesign
+{.overview-img align=left}
+The **landingGearDesign** module calculates characteristic parameters for the landing gear of entire aircraft project.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## propulsionIntegration
+{.overview-img align=left}
+The **propulsionIntegration** module integrates the propulsion system to the aircraft.
+This occurs in relation to the user settings (e.g. integration of the propulsion on the wing or fuselage, ...).
+Depending on the location of the integration, the tool calculates the nacelle and pylon geometry.
+If a geometry already exists, it is possible to scale it.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## systemsDesign
+{.overview-img align=left}
+The **systemsDesign** is part of the tool chain in the UNICADO aircraft design environment.
+It dimensions ATA chapter systems in terms of mass and energy requirement divided by hydraulic- electric- and bleed air energy requirement.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
+
+## wingDesign
+{.overview-img align=left}
+The wing design module calculates characteristic parameter of the aircraft main wing.
+{.overview-item}
+
+|Module Version|Language|License|Documentation|
+|:---:|:---:|:---:|---|
+|2.1.0|:simple-cplusplus: |GPLv3|[Link]()|
+
+---
\ No newline at end of file
diff --git a/docs/partners.md b/docs/partners.md
new file mode 100644
index 0000000000000000000000000000000000000000..e69de29bb2d1d6434b8b29ae775ad8c2e48c5391
diff --git a/docs/workflow.md b/docs/workflow.md
new file mode 100644
index 0000000000000000000000000000000000000000..5d37eb59798e3290a090d89c1199bd3bc71622de
--- /dev/null
+++ b/docs/workflow.md
@@ -0,0 +1,24 @@
+---
+title: Worfkflow
+summary: Introduces the UNICADO workflow in RCE
+authors:
+ - Sebastian Oberschwendtner
+date: 2023-09-08
+---
+
+## RCE
+
+## Workflow
+The workflow looks like this:
+<figure markdown>
+ {width="800"}
+ <figcaption>UNICADO Workflow</figcaption>
+</figure>
+
+## Tigl Viewer
+The aicrafts can be view by the Tigl Viewer when they are converted to the **CPACS** format:
+
+<figure markdown>
+ {width="800"}
+ <figcaption>Aircraft shown in Tigl Viewer</figcaption>
+</figure>
\ No newline at end of file
diff --git a/mkdocs.yml b/mkdocs.yml
index 0a54a09618c5a172b213d08911255a4f8f19403a..3a3da5ec54b1a39f1ba13e83ea31b7e540d5fea6 100644
--- a/mkdocs.yml
+++ b/mkdocs.yml
@@ -21,23 +21,105 @@ site_name: UNICADO
markdown_extensions:
- attr_list
- admonition
- - pymdownx.details
- - pymdownx.superfences
+ - md_in_html
- toc:
- permalink: "#"
+ permalink: '#'
+ - pymdownx.tabbed:
+ alternate_style: true
- pymdownx.emoji:
- emoji_index: !!python/name:materialx.emoji.twemoji
- emoji_generator: !!python/name:materialx.emoji.to_svg
+ emoji_index: !!python/name:material.extensions.emoji.twemoji
+ emoji_generator: !!python/name:material.extensions.emoji.to_svg
+ - pymdownx.highlight:
+ anchor_linenums: true
+ line_spans: __span
+ pygments_lang_class: true
+ - pymdownx.details
+ - pymdownx.superfences
+ - pymdownx.inlinehilite
+ - pymdownx.snippets
+ - pymdownx.critic
+ - pymdownx.caret
+ - pymdownx.keys
+ - pymdownx.mark
+ - pymdownx.tilde
+
+
+
+extra_javascript:
+ - assets/javascripts/katex.js
+ - https://cdnjs.cloudflare.com/ajax/libs/KaTeX/0.16.7/katex.min.js
+ - https://cdnjs.cloudflare.com/ajax/libs/KaTeX/0.16.7/contrib/auto-render.min.js
+
+extra_css:
+ - assets/css/unicado.css
+ - https://cdnjs.cloudflare.com/ajax/libs/KaTeX/0.16.7/katex.min.css
+
+# === Plugins ===
+plugins:
+ - glightbox
# === Theme configuration ===
theme:
name: material
favicon: assets/favicon.png
- logo: assets/images/icon.png
+ logo: assets/images/logos/unicado-icon.png
palette:
scheme: slate
primary: blue grey
accent: lime
features:
+ - navigation.path
- navigation.top
+ - navigation.tabs
- toc.follow
+
+# === Page Tree ===
+nav:
+ - 'Home':
+ - 'index.md'
+ - 'description.md'
+ - 'workflow.md'
+ - 'partners.md'
+ - 'Module Overview':
+ - 'modules/overview.md'
+ - 'Aircraft Design':
+ - 'modules/sizing.md'
+ - 'modules/analysis.md'
+ - 'modules/libraries.md'
+ - 'modules/additional-software.md'
+ - 'Getting Started':
+ - 'getting-started/installation.md'
+ - 'getting-started/takeoff.md'
+ - 'Developer':
+ - 'How to Contribute': 'developer/contribute.md'
+ - 'Build Environment':
+ - 'IDE Setup': 'developer/ide-setup.md'
+ - 'C++ Environment': 'developer/environment-cpp.md'
+ - 'Python Environment': 'developer/environment-python.md'
+ - 'Build Instructions':
+ - 'Prerequisites': 'developer/prerequisites.md'
+ - 'Building C++ Modules': 'developer/build-cpp.md'
+ - 'Build Python Modules': 'developer/build-python.md'
+ - 'Libraries': 'developer/including-libraries.md'
+ - 'Style Guide':
+ - 'C++': 'developer/style/cpp.md'
+ - 'Python': 'developer/style/python.md'
+ - 'Aircraft Exchange File':
+ - 'General': 'aircraft-xml/general.md'
+ - 'MassesAndLoadings': 'aircraft-xml/masses.md'
+ - 'Geometry': 'aircraft-xml/geometry.md'
+ - 'Structure': 'aircraft-xml/structure.md'
+ - 'Accommodation': 'aircraft-xml/accommodation.md'
+ - 'Propulsion': 'aircraft-xml/propulsion.md'
+ - 'Systems': 'aircraft-xml/systems.md'
+ - 'Aerodynamics': 'aircraft-xml/aerodynamics.md'
+ - 'StabilityAndControlCharacteristics': 'aircraft-xml/stability.md'
+ - 'Performance': 'aircraft-xml/performance.md'
+ - 'MonetaryValues': 'aircraft-xml/monetary.md'
+ - 'EcologicalValues': 'aircraft-xml/ecological.md'
+ - 'Requirements': 'aircraft-xml/requirements.md'
+ - 'DesignSpecification': 'aircraft-xml/specification.md'
+ - 'About':
+ - 'license.md'
+ - 'contact.md'
+ - 'impressum.md'
diff --git a/scripts/CSR-02.xml b/scripts/CSR-02.xml
new file mode 100644
index 0000000000000000000000000000000000000000..e79520e4d32219dab0ba3b909b1e934b6d9c4b38
--- /dev/null
+++ b/scripts/CSR-02.xml
@@ -0,0 +1,3767 @@
+<AcftExchangeFile>
+ <General Desc="Allgemeine Angaben">
+ <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
+ <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-02</Model>
+ </General>
+ <MassesAndLoadings Desc="-">
+ <MassBreakdown Desc="Mass breakdown">
+ <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
+ <Mass ToolLevel="1" Unit="kg">8288.967026</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ <CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4">
+ <Mass ToolLevel="1" Unit="kg">6063.492374</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ <EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor>
+ <EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor>
+ <EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor>
+ </CenterWing>
+ <WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8">
+ <Mass ToolLevel="1" Unit="kg">2225.474652</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
+ <Mass ToolLevel="1" Unit="kg">282.297482</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </FixedLeadingEdge>
+ <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
+ <Mass ToolLevel="1" Unit="kg">380.8095925</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </MovableLeadingEdge>
+ <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
+ <Mass ToolLevel="1" Unit="kg">546.1954554</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </FixedTrailingEdge>
+ <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
+ <Mass ToolLevel="1" Unit="kg">1016.172122</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </MovableTrailingEdge>
+ </WingLEandTE>
+ <Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9">
+ <Mass ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </Miscellaneous>
+ </Wing>
+ <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">8482.604033</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Fuselage>
+ <Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements">
+ <Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1325.468005</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.95934635</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
+ </RefPoint>
+ <Tailplane Desc="Airbus Chapter 13">
+ <Mass ToolLevel="1" Unit="kg">759.3554913</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">34.25726239</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
+ </RefPoint>
+ </Tailplane>
+ <Fin Desc="Airbus Chapter 14">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">566.1125139</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.55973642</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Item>
+ </RefPoint>
+ </Fin>
+ </Empennage>
+ <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2600.672138</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.45985449</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.413319125</h_Item>
+ </RefPoint>
+ <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">390.1008207</Mass>
+ <RefPoint Desc="Position of NoseGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">1.947356458</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.978883883</h_Item>
+ </RefPoint>
+ <Strut>
+ <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+ <RefPoint Desc="position of strut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Strut>
+ <SupportStrut>
+ <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+ <RefPoint Desc="position of suppStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SupportStrut>
+ <WheelGroupConnection>
+ <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+ <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WheelGroupConnection>
+ <WheelGroup>
+ <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+ <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+ <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+ <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+ </WheelGroup>
+ </Gear>
+ <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
+ <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.313513579</h_Item>
+ </RefPoint>
+ <Strut>
+ <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+ <RefPoint Desc="position of strut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Strut>
+ <SupportStrut>
+ <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+ <RefPoint Desc="position of suppStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SupportStrut>
+ <WheelGroupConnection>
+ <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+ <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WheelGroupConnection>
+ <WheelGroup>
+ <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+ <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+ <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+ <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+ </WheelGroup>
+ </Gear>
+ <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1105.285659</Mass>
+ <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">17.84441297</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">-1.313513579</h_Item>
+ </RefPoint>
+ <Strut>
+ <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+ <RefPoint Desc="position of strut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Strut>
+ <SupportStrut>
+ <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+ <RefPoint Desc="position of suppStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SupportStrut>
+ <WheelGroupConnection>
+ <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+ <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WheelGroupConnection>
+ <WheelGroup>
+ <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+ <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+ <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+ <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+ </WheelGroup>
+ </Gear>
+ <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <Strut>
+ <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+ <RefPoint Desc="position of strut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Strut>
+ <SupportStrut>
+ <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+ <RefPoint Desc="position of suppStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SupportStrut>
+ <WheelGroupConnection>
+ <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+ <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WheelGroupConnection>
+ <WheelGroup>
+ <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+ <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+ <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+ <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+ </WheelGroup>
+ </Gear>
+ <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
+ <Mass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <Strut>
+ <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+ <RefPoint Desc="position of strut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Strut>
+ <SupportStrut>
+ <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+ <RefPoint Desc="position of suppStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SupportStrut>
+ <WheelGroupConnection>
+ <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+ <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+ <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WheelGroupConnection>
+ <WheelGroup>
+ <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+ <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+ <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+ <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+ </WheelGroup>
+ </Gear>
+ </LandingGear>
+ <Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">1302.156306</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.87054623</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.53285849</h_Item>
+ </RefPoint>
+ </Pylons>
+ <PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit">
+ <Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">8513.660953</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.78507499</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.958381704</h_Item>
+ </RefPoint>
+ <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">4009.674109</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </OtherSystems>
+ <Prop Desc="Propeller mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Prop>
+ </Engine>
+ <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">4009.674109</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2748.88918</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">713.6948535</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">547.0900758</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.66216673</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.49297931</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-3.072020922</h_Item>
+ </RefPoint>
+ </OtherSystems>
+ <Prop Desc="Propeller mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Prop>
+ </Engine>
+ <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </OtherSystems>
+ <Prop Desc="Propeller mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Prop>
+ </Engine>
+ <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <EngineDry Desc="Engine dry mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </EngineDry>
+ <Nacelle Desc="Nacelle mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Nacelle>
+ <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </OtherSystems>
+ <Prop Desc="Propeller mass">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Prop>
+ </Engine>
+ <BleedAirSystem Desc="Airbus Chapter 21, ATA36">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">172.6795332</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
+ </RefPoint>
+ </BleedAirSystem>
+ <EngineControls Desc="Airbus Chapter 22">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </EngineControls>
+ <FuelSystem Desc="Airbus Chapter 25, ATA28">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">321.6332021</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">17.1682343</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.030900284</h_Item>
+ </RefPoint>
+ </FuelSystem>
+ </PowerUnit>
+ <Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
+ <Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5355.445849</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.39637449</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-0.5741904671</h_Item>
+ </RefPoint>
+ <APU Desc="Airbus Chapter 30, ATA49">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">254.7995941</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">35.65115779</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </APU>
+ <HydraulicGeneration Desc="Airbus Chapter 31, ATA 29">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">184.4172612</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
+ </RefPoint>
+ </HydraulicGeneration>
+ <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">805.6612438</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
+ </RefPoint>
+ </HydraulicDistribution>
+ <AirConditioning Desc="Airbus Chapter 33, ATA21">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">717.7462397</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
+ </RefPoint>
+ </AirConditioning>
+ <DeIcing Desc="Airbus Chapter 34, ATA30">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">42.30906964</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </DeIcing>
+ <FireProtection Desc="Airbus Chapter 35, ATA26">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">94.97439103</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </FireProtection>
+ <FlightControls Desc="Airbus Chapter 36, ATA27">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">711.5018356</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.05413654</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Item>
+ </RefPoint>
+ <Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">43.35817647</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Roll>
+ <Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">94.98684287</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Yaw>
+ <Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">33.35895545</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Pitch>
+ <MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">64.77541722</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </MovableHorizontalTail>
+ <Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">147.1812978</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Flaps>
+ <SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.5">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">39.74320013</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </SpoilersAirbrakesLiftdumpers>
+ <Slats Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.6">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">145.7975785</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Slats>
+ <CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">142.3003671</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </CommonInstallation>
+ </FlightControls>
+ <Instruments Desc="Airbus Chapter 37, ATA31">
+ <Mass ToolLevel="1" Unit="kg">85.52867064</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.125269051</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Instruments>
+ <AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22">
+ <Mass ToolLevel="1" Unit="kg">138.9840898</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </AutomaticFlightSystem>
+ <Navigation Desc="Airbus Chapter 39, ATA34">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">566.627443</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Navigation>
+ <Communication Desc="Airbus Chapter 40, ATA23">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">277.9681796</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Communication>
+ <ElectricalGeneration Desc="Airbus Chapter 41, ATA24">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">779.0134574</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </ElectricalGeneration>
+ <ElectricalDistribution Desc="Airbus Chapter 42, ATA24">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">695.9143735</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </ElectricalDistribution>
+ </Systems>
+ <Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings">
+ <Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3108.708964</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <Furnishing Desc="Airbus Chapter 50, ATA25">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">2452.022285</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Furnishing>
+ <FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </FixedEmergencyOxygen>
+ <Lighting Desc="Airbus Chapter 52, ATA33">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">268.2126788</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </Lighting>
+ <WaterInstallation Desc="Airbus Chapter 53, ATA38">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.88739053</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </WaterInstallation>
+ </Furnishings>
+ <OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items">
+ <Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3331.623637</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.6792334</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ <OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">1581.073637</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.71467966</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </OperatorEquipment>
+ <OperationalEquipment Desc="Airbus Chapter 61 (movable equipment)">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.84084522</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </OperationalEquipment>
+ </OperatorsItems>
+ <NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements">
+ <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+ <RefPoint Desc="position of mass item to global point of reference">
+ <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+ <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+ <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+ </RefPoint>
+ </NotAllocated>
+ </MassBreakdown>
+ <MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM>
+ <MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">66724.81066</MLM>
+ <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">79148.59668</MTOM>
+ <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
+ <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38977.68327</MME>
+ <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">42309.30691</OME>
+ <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">62309.30691</MZFM>
+ <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
+ <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">32478.96446</MaximumUsableFuel>
+ <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">625.8366729</WingLoading>
+ <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3320609465</ThrustToWeight>
+ <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
+ <MassMomentsOfInertia Desc="Mass moment of inertia (MMoI)">
+ <DesignPoint Desc="MMoI at Designpoint">
+ <Jxx Desc="MMoI x-axis" ToolLevel="1" Unit="kg*m2">1200828.866</Jxx>
+ <Jyy Desc="MMoI y-axis" ToolLevel="1" Unit="kg*m2">3139142.531</Jyy>
+ <Jzz Desc="MMoI z-axis" ToolLevel="1" Unit="kg*m2">4166372.541</Jzz>
+ <Jxy Desc="MMoI xy-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxy>
+ <Jxz Desc="MMoI xz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jxz>
+ <Jyz Desc="MMoI yz-axis (deviation)" ToolLevel="1" Unit="kg*m2">0</Jyz>
+ </DesignPoint>
+ </MassMomentsOfInertia>
+ <CentreOfGravityRange Desc="Schwerpunktsgrenzen">
+ <TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug">
+ <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7482016769</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.80339635</r>
+ <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+ </TrimRefPt>
+ <ForwardLimit Desc="Vorderste Schwerpunktlage">
+ <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9750336151</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.67440503</r>
+ <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+ </ForwardLimit>
+ <AftLimit Desc="Hinterste Schwerpunktlage">
+ <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9992954046</h>
+ <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.88886532</r>
+ <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+ </AftLimit>
+ </CentreOfGravityRange>
+ </MassesAndLoadings>
+ <Geometry Desc="Geometriebeschreibung">
+ <UsedElements Desc="Liste der verwendeten Geometrieelemente">
+ <LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces>
+ <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface>
+ <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface>
+ <VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces>
+ <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface>
+ <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface>
+ <Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages>
+ <Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage>
+ <Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle>
+ <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle>
+ <Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon>
+ <Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon>
+ <Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears>
+ <Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear>
+ <Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear>
+ <Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear>
+ <Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear>
+ <Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear>
+ </UsedElements>
+ <LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing">
+ <SurfaceRefPoint Desc="position of wing to global point of reference">
+ <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.51238234</r_Surface>
+ <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.27103384</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of lifting surface geometry">
+ <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
+ <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
+ <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface>
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints>
+ <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
+ <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_15.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_12.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">7.083508401</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.434391811</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.199184069</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_12.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\F15_11.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.434391811</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.053794453</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">12.1314295</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+ <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1168298891</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2054149445</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices>
+ <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+ <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1168298891</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </LEDevice>
+ </ControlDeviceSetup>
+ </HalfSurfaceDescription>
+ <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
+ <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+ <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+ <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+ <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </LEDevice>
+ </ControlDeviceSetup>
+ </HalfSurfaceDescription>
+ </SurfaceParameters>
+ </LiftingSurface>
+ <LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser">
+ <SurfaceRefPoint Desc="position of wing to global point of reference">
+ <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.6591417</r_Surface>
+ <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.654512598</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of lifting surface geometry">
+ <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
+ <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
+ <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.250900566</i_Surface>
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
+ <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.992016088</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.123933623</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.439701701</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+ <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+ <Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+ <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+ <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </LEDevice>
+ </ControlDeviceSetup>
+ </HalfSurfaceDescription>
+ <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
+ <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
+ <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </HalfSurfaceSegment>
+ <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+ <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+ <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+ <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+ <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+ </DeflectionAngle>
+ </LEDevice>
+ </ControlDeviceSetup>
+ </HalfSurfaceDescription>
+ </SurfaceParameters>
+ </LiftingSurface>
+ <VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin">
+ <SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.86369528</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.654512598</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of vertical surface geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.787462516</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.531274612</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.952800274</s_Segment>
+ <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+ <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+ <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+ <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+ </SurfaceSegment>
+ <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+ <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
+ <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+ <Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type>
+ <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
+ <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+ <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+ <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+ <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+ <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+ <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+ </DeflectionAngle>
+ </TEDevice>
+ </ControlDeviceSetup>
+ </SurfaceParameters>
+ </VerticalSurface>
+ <Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage">
+ <FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference">
+ <r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage>
+ <y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage>
+ <h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage>
+ </FuselageRefPoint>
+ <FuselageParameters Desc="parametric description of the fuselage">
+ <NoseDescription>
+ <NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments>
+ <TipSegment>
+ <h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5232505048</h_Tip>
+ </TipSegment>
+ <NoseSegment ID="1">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6219072875</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.647944796</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06445732892</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5232505048</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="2">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.232171749</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.283759313</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.1933719868</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4278783272</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="3">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.81877794</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.894925056</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3222866446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3362034659</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="4">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.368913086</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.468092813</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4512013025</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2502283023</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="5">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.868421677</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.988514422</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.5801159603</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1721650609</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="6">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.301028172</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.439232935</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7090306182</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1045572839</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="7">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.6471193</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.799813925</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.837945276</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05047013554</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="8">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.881644273</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.044157799</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.9668599339</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01381855438</deltah_Segment>
+ </NoseSegment>
+ <NoseSegment ID="9">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.095774592</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment>
+ </NoseSegment>
+ </NoseDescription>
+ <MidSectionDescription>
+ <MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments>
+ <MidSectionSegment ID="1">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136281495</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">16.76076782</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
+ </MidSectionSegment>
+ <MidSectionSegment ID="2">
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
+ </MidSectionSegment>
+ </MidSectionDescription>
+ <TailDescription>
+ <TailSegments Desc="No of tail segments" ToolLevel="1">7</TailSegments>
+ <TailSegment ID="1">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.074891643</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.03069492579</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="2">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.970066</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.889781167</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.1232501637</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="3">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.892703799</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.578053688</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.2791139033</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="4">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.618301624</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.143415874</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.4964328104</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="5">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.142809701</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.681089784</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.72542446</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.7275958556</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="6">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.985033</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.754173041</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.191054227</deltah_Segment>
+ </TailSegment>
+ <TailSegment ID="7">
+ <SegmentPointData ToolLevel="1">geometryData\fuselage.dat</SegmentPointData>
+ <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</w_Segment>
+ <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.827256299</h_Segment>
+ <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.459300377</l_Segment>
+ <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.654512598</deltah_Segment>
+ </TailSegment>
+ </TailDescription>
+ </FuselageParameters>
+ </Fuselage>
+ <Nacelle Desc="Beschreibung der inneren rechten Triebwerksgondel" ID="InnerRightWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">5.49297931</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">20</Points>
+ <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="3">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="4">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.30681609</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-5.49297931</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">20</Points>
+ <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.355350639</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">geometryData\nacelle.dat</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">geometryData\nacelle.dat</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.471029026</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.861475931</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.6776753197</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="3">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="4">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">geometryData\nacelle.dat</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.289180745</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.976823221</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+ <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der aeusseren linken Triebwerksgondel" ID="OuterLeftWingNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+ <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der rechten Hecktriebwerksgondel" ID="RightFuselageNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+ <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+ <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle">
+ <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+ <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+ <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+ <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+ </NacelleRefPoint>
+ <NacelleParameters Desc="parametric description of the nacelle">
+ <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+ <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+ <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+ <InletSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+ <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+ <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+ </InletSegment>
+ <NacelleSegment ID="1">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <NacelleSegment ID="2">
+ <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+ <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+ <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+ <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+ <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+ <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+ <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+ </NacelleSegment>
+ <ExitSegment>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+ <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+ </ExitSegment>
+ </NacelleParameters>
+ <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+ </Nacelle>
+ <Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.57788621</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.49297931</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.83066751</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.57788621</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.49297931</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-3.072020922</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.252841535</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.066051918</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.201819891</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">geometryData\airfoilData\n0012.dat</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.066051918</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.110599868</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.8012132607</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.83066751</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon">
+ <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+ <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+ <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+ <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+ </SurfaceRefPoint>
+ <SurfaceParameters Desc="Parametric description of pylon geometry">
+ <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+ <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+ <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+ <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+ <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+ <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+ <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+ <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+ <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+ <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+ </SurfaceSegment>
+ </SurfaceParameters>
+ </Pylon>
+ <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
+ <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+ <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.480695762</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.978883883</h_Gear>
+ </GearRefPoint>
+ <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+ <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.480695762</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-5.04556249</h_Wheelgroup>
+ </WheelGroupRefPoint>
+ <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter>
+ <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+ <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+ <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+ <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+ <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+ </HingeAxis>
+ <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
+ <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+ <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack>
+ <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+ <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+ <Wheel Desc="Beschreibung des Rades">
+ <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter>
+ <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth>
+ <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter>
+ </Wheel>
+ </Gear>
+ <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
+ <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+ <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.84441297</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</h_Gear>
+ </GearRefPoint>
+ <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+ <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.80664751</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.257464797</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</h_Wheelgroup>
+ </WheelGroupRefPoint>
+ <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
+ <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+ <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+ <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+ <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+ <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+ </HingeAxis>
+ <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle>
+ <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+ <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
+ <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+ <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+ <Wheel Desc="Beschreibung des Rades">
+ <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
+ <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
+ <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
+ </Wheel>
+ </Gear>
+ <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
+ <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+ <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.84441297</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.313513579</h_Gear>
+ </GearRefPoint>
+ <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+ <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.80664751</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.257464797</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.80426249</h_Wheelgroup>
+ </WheelGroupRefPoint>
+ <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
+ <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+ <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+ <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+ <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+ <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+ </HingeAxis>
+ <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
+ <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+ <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
+ <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+ <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+ <Wheel Desc="Beschreibung des Rades">
+ <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
+ <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
+ <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
+ </Wheel>
+ </Gear>
+ <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
+ <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+ <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
+ </GearRefPoint>
+ <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+ <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
+ </WheelGroupRefPoint>
+ <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
+ <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
+ <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+ <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+ <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+ <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+ </HingeAxis>
+ <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
+ <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+ <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
+ <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
+ <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
+ <Wheel Desc="Beschreibung des Rades">
+ <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
+ <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
+ <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
+ </Wheel>
+ </Gear>
+ <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
+ <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+ <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
+ <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+ <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
+ </GearRefPoint>
+ <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+ <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
+ <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+ <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
+ </WheelGroupRefPoint>
+ <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
+ <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
+ <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+ <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+ <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+ <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+ </HingeAxis>
+ <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
+ <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+ <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
+ <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
+ <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
+ <Wheel Desc="Beschreibung des Rades">
+ <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
+ <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
+ <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
+ </Wheel>
+ </Gear>
+ </Geometry>
+ <Structure Desc="Strukturdaten"></Structure>
+ <Accommodation Desc="Kabineneinrichtung">
+ <PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal>
+ <FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew>
+ <CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew>
+ <Seats Desc="Description of seats">
+ <NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">2</NoOfSeatTypes>
+ <seat Desc="Description of seat" ID="1">
+ <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType>
+ <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
+ </seatConfiguration>
+ <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
+ <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
+ </seat>
+ <seat Desc="Description of seat" ID="2">
+ <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType>
+ <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
+ </seatConfiguration>
+ <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
+ <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
+ <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
+ </seatConfiguration>
+ <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
+ <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
+ </seat>
+ </Seats>
+ <Galleys Desc="Description of galleys">
+ <NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes>
+ <Gal Desc="Description of galley" ID="1">
+ <nameGalley Desc="Name of galley" ToolLevel="1">large</nameGalley>
+ <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
+ <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass>
+ <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power>
+ </Gal>
+ <Gal Desc="Description of galley" ID="2">
+ <nameGalley Desc="Name of galley" ToolLevel="1">small</nameGalley>
+ <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
+ <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass>
+ <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power>
+ </Gal>
+ </Galleys>
+ <Lavatories Desc="Description of lavatories">
+ <NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes>
+ <Lav Desc="Description of lavatory" ID="1">
+ <nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory>
+ <NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories>
+ <mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass>
+ </Lav>
+ </Lavatories>
+ <Cabin Desc="Beschreibung der Kabine">
+ <V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">186.1462316</V_AirConditioned>
+ <CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks>
+ <CabinDeck Desc="Parameter eines Kabinendecks" ID="1">
+ <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">97.50130651</A_CabinDeck>
+ <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
+ <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.63012573</w_CabinDeck>
+ <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.85893376</l_CabinDeck>
+ <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">184.2960557</V_CabinDeck>
+ <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck>
+ <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes>
+ <Class Desc="Definition der Klasse" ID="1">
+ <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">5.983021821</x_center>
+ </Class>
+ <Class Desc="Definition der Klasse" ID="2">
+ <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.4124887</x_center>
+ </Class>
+ </CabinDeck>
+ </Cabin>
+ <Cargo Desc="Beschreibung des Frachtraums">
+ <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">35.92426606</V_Cargo>
+ <CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks>
+ <CargoDeck Desc="Parameter eines Frachtdecks" ID="1">
+ <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">56.63668783</A_CargoDeck>
+ <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
+ <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.280233538</w_CargoDeck>
+ <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">17.26605352</l_CargoDeck>
+ <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">36.40649695</V_CargoDeck>
+ <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.7695477</V_BulkCargo>
+ <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments>
+ <Compartment Desc="Definition des Compartments" ID="1">
+ <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.84</Length>
+ <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center>
+ </Compartment>
+ <Compartment Desc="Definition des Compartments" ID="2">
+ <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.37</Length>
+ <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">18.82863715</x_center>
+ </Compartment>
+ </CargoDeck>
+ </Cargo>
+ </Accommodation>
+ <Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)">
+ <NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes>
+ <Engine Desc="Triebwerks-/Motortyp" ID="1">
+ <TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine>
+ <EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel>
+ <NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines>
+ <ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.168175939</ScaleEngines>
+ <ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow>
+ <EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">engineData\V2527-A5\V2527-A5.xml</EngineDataFile>
+ <JetEngineData Desc="Jet spezifische Triebwerksdaten">
+ <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">128.8646365</SeaLevelStaticThrust>
+ <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.743365695</FanDiameter>
+ </JetEngineData>
+ <TurbopropEngineData Desc="Prop spezifische Triebwerksdaten">
+ <Prop Desc="Propellerdaten">
+ <PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter>
+ <PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades>
+ <SegmentPointData ToolLevel="1">0</SegmentPointData>
+ <Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch>
+ <Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness>
+ </Prop>
+ <P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp>
+ </TurbopropEngineData>
+ <EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk">
+ <w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.976823221</w_Engine>
+ <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.289180745</h_Engine>
+ <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.710701279</l_Engine>
+ </EngineDimensions>
+ <NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0">
+ <InnerNacelle>
+ <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
+ <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
+ <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
+ <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
+ <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
+ <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
+ </InnerNacelle>
+ <OuterNacelle>
+ <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
+ <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
+ <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
+ <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
+ <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
+ <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
+ </OuterNacelle>
+ </NacelleRescaling>
+ <ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks">
+ <EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+deltaISA(Requirements/DesignMission), SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">127.3858501</EquivalentThrust>
+ <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">128.8646365</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.316357232</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01021503857</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9783203125</N1>
+ </MaximumTakeOff>
+ <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+deltaISA(Requirements/DesignMission) und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">101.9086801</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.329201509</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01304306471</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.9734765625</N1>
+ </MaximumGoAround>
+ <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+deltaISA(Requirements/DesignMission) bei" Mach="0.8">
+ <MaxThrust Desc="Without Offtakes">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">32.18450048</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5460196217</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01696529738</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.981796875</N1>
+ </MaxThrust>
+ <BucketThrust Desc="Without Offtakes">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4959848906</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01693808075</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</N1>
+ </BucketThrust>
+ <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
+ <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">29.28223674</Thrust>
+ <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.5130623087</FuelFlow>
+ <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01752128136</TSFC>
+ <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.950379375</N1>
+ </BucketThrustOfftakes>
+ </MaximumContinous>
+ </ScaledPerformanceCharacteristics>
+ <UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird">
+ <UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines>
+ <NacelleID ID="1" ToolLevel="1">0</NacelleID>
+ <NacelleID ID="2" ToolLevel="1">0</NacelleID>
+ <NacelleID ID="3" ToolLevel="1">0</NacelleID>
+ <NacelleID ID="4" ToolLevel="1">0</NacelleID>
+ </UsedForNacelles>
+ </Engine>
+ </Propulsion>
+ <Systems>
+ <FuelTank Desc="Tank system Parameters">
+ <CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks>
+ <CentreTank Desc="Centre tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">10541.14749</TankVolume>
+ </CentreTank>
+ <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
+ <WingTank Desc="Wing tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
+ </WingTank>
+ <WingTank Desc="Wing tank description" ID="2">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">15416.66477</TankVolume>
+ </WingTank>
+ <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
+ <TrimTank Desc="Trim tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
+ </TrimTank>
+ <FuselageTanks Desc="No of fuselage tanks" ToolLevel="1">0</FuselageTanks>
+ <FuselageTank Desc="Fuselage tank description" ID="1">
+ <TankVolume Desc="Tank volume" ToolLevel="1" Unit="l">0</TankVolume>
+ </FuselageTank>
+ <TotalFuelVolume Desc="Total fuel volume of all tanks" ToolLevel="1" Unit="l">41374.47702</TotalFuelVolume>
+ </FuelTank>
+ <ATA21_EnvironmentalControlSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.37098678</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.31382376</BleedAir>
+ </DesignPower>
+ <AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax>
+ <Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation>
+ </ATA21_EnvironmentalControlSystem>
+ <ATA22_AutoFlight>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA22_AutoFlight>
+ <ATA23_Communication>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA23_Communication>
+ <ATA24_ElectricSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA24_ElectricSystem>
+ <ATA25_Furnishing>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA25_Furnishing>
+ <ATA26_FireProtection>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA26_FireProtection>
+ <ATA27_FlightControlSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">93.56406668</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA27_FlightControlSystem>
+ <ATA28_FuelSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">12.23167268</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA28_FuelSystem>
+ <ATA29_HydraulicSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.451202472</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ <Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure>
+ </ATA29_HydraulicSystem>
+ <ATA30_IceRainProtection>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.6613272863</BleedAir>
+ </DesignPower>
+ </ATA30_IceRainProtection>
+ <ATA31_Instrumentation>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA31_Instrumentation>
+ <ATA32_LandingGear>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">74.97503685</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA32_LandingGear>
+ <ATA33_Lights>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.884251516</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA33_Lights>
+ <ATA34_Navigation>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA34_Navigation>
+ <ATA35_Oxygen>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+ </DesignPower>
+ </ATA35_Oxygen>
+ <ATA36_BleedAir>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1039553182</BleedAir>
+ </DesignPower>
+ </ATA36_BleedAir>
+ <ATA49_APU>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir>
+ </DesignPower>
+ </ATA49_APU>
+ <ATA70_PropulsionSystem>
+ <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+ <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-205.4781816</Electric>
+ <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-181.0078664</Hydraulic>
+ <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.188533015</BleedAir>
+ </DesignPower>
+ </ATA70_PropulsionSystem>
+ </Systems>
+ <Aerodynamics Desc="Aerodynamik">
+ <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">16.46037111</LoverD_Cruise>
+ <LiftCoefficients Desc="Auftriebsbeiwerte">
+ <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5381848981</C_L_design>
+ <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.916185004</C_LmaxLanding>
+ <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.515329503</C_LmaxT-O>
+ <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.528</C_LoptimumCruise>
+ <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.5626638406</C_L_opt_wing>
+ <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03466354382</C_L_opt_stab>
+ <C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll>
+ </LiftCoefficients>
+ <DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)">
+ <C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03207704106</C_D_total>
+ <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.009803808575</C_D_ind>
+ <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
+ <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01972511904</C_D_visc_total>
+ <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00660550988</C_D_visc_wing>
+ <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001454379701</C_D_visc_stab>
+ <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001569261547</C_D_visc_fin>
+ <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006412233533</C_D_visc_fus>
+ <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001743616971</C_D_visc_nac>
+ <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.001940117406</C_D_visc_misc>
+ </C_D_visc>
+ <C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-">
+ <C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.002548113448</C_D_wave_total>
+ <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.002547491352</C_D_wave_wing>
+ <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">6.220952302e-07</C_D_wave_stab>
+ </C_D_wave>
+ <EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor>
+ </DragCoefficients>
+ <MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)">
+ <C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">1.138318599e-05</C_M_total>
+ </MomentCoefficients>
+ <Polar Desc="Flugzeugpolare">
+ <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">aeroData\CSR-02_polar.xml</PolarFile>
+ <Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration>
+ <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration>
+ </Polar>
+ <ReferenceValues Desc="Aerodynamische Bezugsgroessen">
+ <b Desc="Total wing span" ToolLevel="1" Unit="m">34.66122714</b>
+ <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.402512853</MAC>
+ <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">126.463228</S_ref>
+ </ReferenceValues>
+ <MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor>
+ </Aerodynamics>
+ <StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit">
+ <Stabiliser>
+ <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.017690098</VolumeCoefficient>
+ <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.94519006</S_ref>
+ </Stabiliser>
+ <VerticalTail>
+ <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.09489408521</VolumeCoefficient>
+ <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">25.44285876</S_ref>
+ </VerticalTail>
+ </StabilityAndControlCharacteristics>
+ <Performance Desc="Flugleistungen">
+ <Range Desc="Reichweiten">
+ <Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3246.670783</Range_maxPayloadatMTOM>
+ <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">10458.2771</Range_maxFuelatMTOM>
+ <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">4360.32531</Payload_maxFuelatMTOM>
+ <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">10709.69495</Range_maxFuelEmpty>
+ </Range>
+ <Speed Desc="Fluggeschwindigkeiten">
+ <M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise>
+ <M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating>
+ <V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating>
+ <M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive>
+ <V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive>
+ <V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">154.8031322</V_s1g>
+ </Speed>
+ <Altitudes Desc="Flughoehen">
+ <h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise>
+ <h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified>
+ <h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">11713.23959</h_maxOperating>
+ <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">11763.23474</h_maxCeiling>
+ <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">6608.028951</h_maxOEI>
+ </Altitudes>
+ <Climb Desc="Climb Performance">
+ <TTC_Design Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_Design>
+ <TTC_ISA Desc="Time needed to climb from 1500ft to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">16.15883289</TTC_ISA>
+ <Time_to_1500ft_ISA Desc="Time needed to climb from BR to 1500ft (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">1.251683745</Time_to_1500ft_ISA>
+ <Time_to_ICA_ISA Desc="Time needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="min">17.41051663</Time_to_ICA_ISA>
+ <Range_to_ICA_ISA Desc="Range needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="NM">101.9061674</Range_to_ICA_ISA>
+ <Fuel_to_ICA_ISA Desc="Fuel mass needed to climb from BR to ICA (ISA+deltaISA(Requirements/DesignMission))" ToolLevel="3" Unit="kg">1715.660845</Fuel_to_ICA_ISA>
+ </Climb>
+ <TakeOff Desc="Start Performance">
+ <TakeOffDistance_Normal Desc="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">660.3942437</TakeOffDistance_Normal>
+ <TakeOffDistance_Normal_Safety Desc="Takeoff distance at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission) (incl. 15 percent safety margin; estimated by calculatePerformance)" ToolLevel="2" Unit="m">1314.175463</TakeOffDistance_Normal_Safety>
+ <BFL Desc="Design takeoff distance - Balanced Field Length at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="m">0</BFL>
+ <TimeToScreenHeight Desc="Time until reaching screen height (35ft) at Sea Level with MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="s">28.99214318</TimeToScreenHeight>
+ <V_LOF Desc="Lift-off speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">126.3711884</V_LOF>
+ <V_1 Desc="Decision Speed at Sea Level for MTOM and ISA+deltaISA(Requirements/DesignMission)-Conditions" ToolLevel="2" Unit="KCAS">0</V_1>
+ <V_2 Desc="Speed at screen height (35 ft)" ToolLevel="2" Unit="KCAS">126.3711884</V_2>
+ <V_FTO Desc="Speed at final takeoff segment (1500 ft)" ToolLevel="2" Unit="KCAS">202.4392823</V_FTO>
+ <ScdSegmentClimbGradient Desc="Climb gradient in second takeoff segment" ToolLevel="2" Unit="%">2.416614712</ScdSegmentClimbGradient>
+ <FinalSegmentClimbGradient Desc="Climb gradient in final takeoff segment" ToolLevel="2" Unit="%">2.416614712</FinalSegmentClimbGradient>
+ </TakeOff>
+ <Landing>
+ <LandingDistance Desc="Landing distance at Sea Level for MLM and (ISA + deltaISA)-Conditions(calculated by missionAnalysis using missionDesign.xml settings)" ToolLevel="3" Unit="m">1373.253939</LandingDistance>
+ <NeededRunwayLength Desc="Needed runway length at Sea Level with MLM and ISA+deltaISA(Requirements/DesignMission)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" ToolLevel="2" Unit="m">1680.105692</NeededRunwayLength>
+ <V_Approach Desc="Final Approach Speed" ToolLevel="2" Unit="KCAS">128.6850003</V_Approach>
+ </Landing>
+ <MissionAnalysis Desc="Missionsanalyse">
+ <DesignMission Desc="Parameter der Design-Mission">
+ <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\missionDesign.xml</MissionFile>
+ <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5009643041</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">19940.80556</Missionfuel>
+ <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">16588.93118</Tripfuel>
+ <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5157969</TaxifuelTakeoff>
+ <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39766495</TaxifuelLdg>
+ <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.94079849</Blocktime>
+ <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.707465156</Flighttime>
+ <Range Desc="Range" ToolLevel="3" Unit="NM">2500.496213</Range>
+ <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">79148.59668</TOM>
+ <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload>
+ <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
+ <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass>
+ <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
+ <Offtakes>
+ <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
+ <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">103.3245182</ShaftPowerTotal>
+ <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
+ </AverageCruiseOfftakes>
+ </Offtakes>
+ <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+ <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5101767772</CL_avg>
+ <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4831782814</CL_min>
+ <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5667676169</CL_max>
+ </LiftCoefficientsCruise>
+ <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+ <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">77451.03811</Mass_TOC>
+ <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">63267.90838</Mass_TOD>
+ </MassesCruise>
+ </DesignMission>
+ <StudyMission Desc="Parameter der Study-Mission">
+ <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionData\missionStudy.xml</MissionFile>
+ <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
+ <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+ <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+ </CruiseStep>
+ <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">6746.530829</Missionfuel>
+ <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3818.187572</Tripfuel>
+ <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">101.5158315</TaxifuelTakeoff>
+ <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">56.39768417</TaxifuelLdg>
+ <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.499139745</Blocktime>
+ <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.265806411</Flighttime>
+ <Range Desc="Range" ToolLevel="3" Unit="NM">500.6435758</Range>
+ <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">62562.32191</TOM>
+ <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload>
+ <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
+ <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass>
+ <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
+ <Offtakes>
+ <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
+ <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">102.8677337</ShaftPowerTotal>
+ <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.8796612188</BleedAirTotal>
+ </AverageCruiseOfftakes>
+ </Offtakes>
+ <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+ <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4609914236</CL_avg>
+ <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4538594196</CL_min>
+ <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4925634903</CL_max>
+ </LiftCoefficientsCruise>
+ <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+ <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">61280.43659</Mass_TOC>
+ <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">59428.93455</Mass_TOD>
+ </MassesCruise>
+ </StudyMission>
+ </MissionAnalysis>
+ <RequirementsChecks>
+ <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionData\missionReq.xml</MissionFile>
+ <TLARs>
+ <TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design>
+ <LDN_Design Checked="1" ToolLevel="2">1</LDN_Design>
+ <V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design>
+ <h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design>
+ <h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating>
+ <h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI>
+ <M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design>
+ <TTC_Design Checked="1" ToolLevel="3">1</TTC_Design>
+ </TLARs>
+ <Certification>
+ <climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment>
+ <climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment>
+ <climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI>
+ <climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO>
+ </Certification>
+ </RequirementsChecks>
+ </Performance>
+ <MonetaryValues Desc="Kosten und Preise">
+ <MonetaryScenario>
+ <AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">0</AirframeEngineeringHours>
+ <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">0</ProductionVolume>
+ </MonetaryScenario>
+ <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">0</Earnings>
+ <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">0</NPV>
+ <Prices Desc="Preise">
+ <PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">0</PriceAirplane>
+ <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0</DiscountRate>
+ </Prices>
+ <LCC Desc="Life Cycle Costs">
+ <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
+ <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">0</NRCTotal>
+ <NRCComponents>
+ <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">0</AirframeEngAndDesign>
+ <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">0</DevSupportAndTesting>
+ <FlightTestAC>
+ <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">0</FlightTestACTotal>
+ <FlightTestACComponents>
+ <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">0</EngineAndAvionics>
+ <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">0</LaborManufacturing>
+ <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">0</MaterialManufacturing>
+ <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">0</Tooling>
+ <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">0</QualityControl>
+ </FlightTestACComponents>
+ </FlightTestAC>
+ <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">0</FlightTestOp>
+ <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
+ </NRCComponents>
+ </NonRecurringCosts>
+ <RecurringCosts Desc="Recurring Costs">
+ <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">0</RCTotal>
+ <RCComponents>
+ <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">0</Wing>
+ <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">0</Fuselage>
+ <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">0</Empennage>
+ <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">0</LandingGear>
+ <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">0</Pylons>
+ <PowerUnit Desc="Costs for all installed engines with systems without pylons">
+ <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">0</PowerUnitTotal>
+ <PowerUnitComponents>
+ <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">0</EquippedEngines>
+ <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">0</Nacelles>
+ <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">0</BleedAirSystem>
+ <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">0</FuelSystem>
+ </PowerUnitComponents>
+ </PowerUnit>
+ <Systems>
+ <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">0</SystemsTotal>
+ <SystemsComponents>
+ <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">0</APU>
+ <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">0</HydraulicSystem>
+ <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">0</AirConditioning>
+ <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">0</DeIcing>
+ <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">0</FireProtection>
+ <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">0</FlightControls>
+ <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">0</Instruments>
+ <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">0</AutomaticFlightSystem>
+ <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">0</Navigation>
+ <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">0</Communication>
+ <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">0</ElectricalSystem>
+ </SystemsComponents>
+ </Systems>
+ <Furnishings>
+ <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">0</FurnishingsTotal>
+ <FurnishingsComponents>
+ <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">0</Furnishing>
+ <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">0</FixedEmergencyOxygen>
+ <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">0</Lighting>
+ <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">0</WaterInstallation>
+ </FurnishingsComponents>
+ </Furnishings>
+ <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">0</OperatorsItems>
+ <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">0</FinalAssembly>
+ </RCComponents>
+ </RecurringCosts>
+ <OperatingCosts>
+ <OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal">
+ <FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">0</FlightsPerYear>
+ <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">0</SeatLoadFactor>
+ </OperatingScenario>
+ <DirectOperatingCosts>
+ <DOC_total Desc="Summe aller DOCComponents (s.u)">
+ <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">0</DOC_year>
+ <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</DOC_FH>
+ <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</DOC_flight>
+ <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</DOC_km>
+ <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</DOC_100ASK>
+ </DOC_total>
+ <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
+ <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">0</COC_year>
+ <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</COC_FH>
+ <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</COC_flight>
+ <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</COC_km>
+ <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</COC_100ASK>
+ </COC_total>
+ <DOCComponents Desc="DOC-Anteile in 100ASK">
+ <Charge Desc="Gebuehren pro 100ASK">
+ <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">0</ChargeTotal>
+ <ChargesComponents>
+ <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0</NavigationCharge>
+ <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0</LandingCharge>
+ <LandingChargeComponents>
+ <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge>
+ <NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge>
+ <ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0</ChargeWithoutEmission>
+ </LandingChargeComponents>
+ <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0</GroundCharge>
+ </ChargesComponents>
+ </Charge>
+ <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0</Depreciation>
+ <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0</Insurance>
+ <Maintenance Desc="Wartungskosten">
+ <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0</MaintenanceTotal>
+ <MaintenanceComponents>
+ <Airframe Desc="Wartungskosten Airframe">
+ <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0</AirframeTotal>
+ <CostComponents>
+ <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
+ <ATA21 Desc="Environmental Control System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA21>
+ <ATA22 Desc="Autoflight">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA22>
+ <ATA23 Desc="Communications">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA23>
+ <ATA24 Desc="Electrical System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA24>
+ <ATA25 Desc="Furnishing">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA25>
+ <ATA26 Desc="Fire Protection">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA26>
+ <ATA27 Desc="Flight Control System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA27>
+ <ATA28 Desc="Fuel System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA28>
+ <ATA29 Desc="Hydraulic System">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA29>
+ <ATA30 Desc="Ice and Rain Protection">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA30>
+ <ATA31 Desc="Instrumentation">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA31>
+ <ATA32 Desc="Landing Gear">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA32>
+ <ATA33 Desc="Lights">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA33>
+ <ATA34 Desc="Navigation">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA34>
+ <ATA35 Desc="Oxygen">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA35>
+ <ATA36 Desc="Pneumatic">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA36>
+ <ATA38 Desc="Water and Waste">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA38>
+ <ATA49 Desc="APU">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA49>
+ <ATA51 Desc="Structure">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA51>
+ <ATA52 Desc="Doors">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA52>
+ <ATA53 Desc="Fuselage">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA53>
+ <ATA54 Desc="Nacelles">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA54>
+ <ATA55 Desc="Stabilizers">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA55>
+ <ATA56 Desc="Windows">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA56>
+ <ATA57 Desc="Wings">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA57>
+ <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
+ <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</TotalCosts>
+ <CostComponents>
+ <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</LabourCosts>
+ <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0</MaterialCosts>
+ </CostComponents>
+ </ATA99>
+ </AirframeComponents>
+ </Airframe>
+ <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0</Engine>
+ </MaintenanceComponents>
+ </Maintenance>
+ <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">0</Fuel>
+ <Crew Desc="Crew Kosten">
+ <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0</CrewTotal>
+ <CrewComponents>
+ <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</FlightCrew>
+ <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0</CabinCrew>
+ </CrewComponents>
+ </Crew>
+ <Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay>
+ </DOCComponents>
+ </DirectOperatingCosts>
+ <IndirectOperatingCosts>
+ <IOC_total Desc="Summe aller IOCComponents (s.u)">
+ <IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">0</IOC_year>
+ <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">0</IOC_FH>
+ <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">0</IOC_flight>
+ <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">0</IOC_km>
+ <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">0</IOC_100ASK>
+ </IOC_total>
+ </IndirectOperatingCosts>
+ </OperatingCosts>
+ <EndOfLifeCosts>
+ <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">0</EOLCTotal>
+ <EOLCTotalComponents>
+ <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">0</TransportToEoLSite>
+ <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">0</DisassemblyAndDismantling>
+ <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">0</Recycling>
+ <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">0</Incineration>
+ <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">0</Landfill>
+ </EOLCTotalComponents>
+ </EndOfLifeCosts>
+ </LCC>
+ </MonetaryValues>
+ <EcologicalValues Desc="Oekologische Bewertung">
+ <Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse">
+ <NoisePathFiles>
+ <Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure>
+ <Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach>
+ </NoisePathFiles>
+ <NoiseCertificationLevels>
+ <LateralPoint>
+ <LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower>
+ <SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL>
+ <Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness>
+ <Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+ <Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness>
+ <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+ </LateralPoint>
+ <FlyoverPoint>
+ <Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover>
+ <SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL>
+ <Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness>
+ <Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+ <Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness>
+ <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+ </FlyoverPoint>
+ <ApproachPoint>
+ <Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach>
+ <SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL>
+ <Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness>
+ <Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+ <Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness>
+ <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+ </ApproachPoint>
+ <CumulativeValues>
+ <EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB>
+ <SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL>
+ <Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness>
+ <Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+ <Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness>
+ <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+ </CumulativeValues>
+ </NoiseCertificationLevels>
+ <CommunityNoiseLevels>
+ <TakeOff>
+ <SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL>
+ <SPLarea>
+ <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
+ <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
+ </SPLarea>
+ <PNLarea>
+ <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
+ <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
+ </PNLarea>
+ <PNLTarea>
+ <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
+ <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
+ </PNLTarea>
+ <EPNLarea>
+ <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
+ <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
+ </EPNLarea>
+ <LoudnessArea>
+ <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
+ <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
+ </LoudnessArea>
+ <TonalityArea>
+ <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
+ <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
+ <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
+ <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
+ </TonalityArea>
+ <SharpnessArea>
+ <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
+ <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
+ </SharpnessArea>
+ <PsychoacousticAnnoyanceArea>
+ <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
+ <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
+ </PsychoacousticAnnoyanceArea>
+ <SELarea Desc="Sound Exposure Level area">
+ <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
+ <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
+ <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
+ <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
+ </SELarea>
+ </TakeOff>
+ <Approach>
+ <SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL>
+ <SPLarea>
+ <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
+ <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
+ </SPLarea>
+ <PNLarea>
+ <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
+ <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
+ </PNLarea>
+ <PNLTarea>
+ <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
+ <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
+ </PNLTarea>
+ <EPNLarea>
+ <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
+ <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
+ </EPNLarea>
+ <LoudnessArea>
+ <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
+ <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
+ </LoudnessArea>
+ <TonalityArea>
+ <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
+ <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
+ <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
+ <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
+ </TonalityArea>
+ <SharpnessArea>
+ <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
+ <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
+ </SharpnessArea>
+ <PsychoacousticAnnoyanceArea>
+ <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
+ <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
+ </PsychoacousticAnnoyanceArea>
+ <SELarea Desc="Sound Exposure Level area">
+ <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
+ <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
+ <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
+ <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
+ </SELarea>
+ </Approach>
+ <CumulativeValues>
+ <EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB>
+ <SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL>
+ <Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness>
+ <Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+ <Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness>
+ <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+ </CumulativeValues>
+ </CommunityNoiseLevels>
+ </Noise>
+ <Emissions>
+ <Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm">
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
+ <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+ <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+ <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+ <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
+ </Development>
+ <Production>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
+ <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+ <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+ <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+ <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
+ </Production>
+ <Operations>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
+ <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+ <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+ <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+ <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
+ <OperationComponents>
+ <ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission">
+ <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</PM10>
+ </ICAO_LTO>
+ <Mission Desc="Environmental analysis of one study mission">
+ <LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)">
+ <Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">0</Total>
+ <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">0</TaxiTime>
+ <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0</TakeOffTime>
+ <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0</ClimbOutTime>
+ <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">0</ApproachTime>
+ </LTOTimes>
+ <LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission">
+ <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0</PM10>
+ </LTO>
+ <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
+ <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">0</H2O>
+ <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">0</SO2>
+ <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">0</HC>
+ <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">0</CO>
+ <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">0</NOx>
+ <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0</PM10>
+ </Cruise>
+ </Mission>
+ </OperationComponents>
+ </Operations>
+ <EndOfLife>
+ <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">0</CO2>
+ <H2O Desc="Wasser" ToolLevel="1" Unit="kg">0</H2O>
+ <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">0</NOx>
+ <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">0</CO>
+ <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">0</SO2>
+ <CH4 Desc="Methan" ToolLevel="1" Unit="kg">0</CH4>
+ <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0</PM10>
+ <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+ <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+ <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+ <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">0</HC>
+ </EndOfLife>
+ </Emissions>
+ <CED Desc="Cumulative Energy Demand">
+ <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">0</CEDTotal>
+ <CEDComponents>
+ <Development Desc="Development" ToolLevel="1" Unit="MJ">0</Development>
+ <Production Desc="Production" ToolLevel="1" Unit="MJ">0</Production>
+ <Operations Desc="Operation" ToolLevel="1" Unit="MJ">0</Operations>
+ <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">0</EndOfLife>
+ </CEDComponents>
+ </CED>
+ <ClimateImpact Desc="Climate Impact due to Aircraft Operation">
+ <ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0</ATR>
+ <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">0</AGTP>
+ <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">0</AGTP100>
+ <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">0</AGWP>
+ <AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100>
+ </ClimateImpact>
+ <AirQuality Desc="Climate Impact due to Aircraft Operation">
+ <ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-">
+ <HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">0</HC>
+ <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0</CO>
+ <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0</NOx>
+ <soot Desc="TF Russ" ToolLevel="1" Unit="-">0</soot>
+ </ToleranceFactors>
+ <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">0</AirQualityIndex>
+ </AirQuality>
+ </EcologicalValues>
+ <Requirements Desc="Designforderungen">
+ <m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload>
+ <m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload>
+ <DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
+ <DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
+ <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
+ <TOFL_Design Desc="Design takeoff distance (Balanced Field Length) at Sea Level with MTOM and (ISA + deltaISA)-Conditions" Unit="m">2122</TOFL_Design>
+ <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+deltaISA)" Unit="min">35</TTC_Design>
+ <ClimbGradients Desc="Steiggradientenforderungen">
+ <secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment>
+ <finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment>
+ <approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO>
+ <approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI>
+ </ClimbGradients>
+ <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
+ <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
+ <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+ <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+ <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
+ </ClimbSpeedSchedule>
+ <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
+ <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+ <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+ </DescentSpeedSchedule>
+ <h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design>
+ <M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design>
+ <LDN_Design Desc="Needed runway length at Sea Level with MLM and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)" Unit="m">2387</LDN_Design>
+ <V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design>
+ <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
+ <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
+ <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
+ <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
+ <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
+ </DesignMission>
+ <StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
+ <DeltaISA Default="0" Desc="Temperature deviation from ISA" Unit="K">0</DeltaISA>
+ <R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design>
+ <m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload>
+ <NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX>
+ <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
+ <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
+ <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+ <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+ <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
+ </ClimbSpeedSchedule>
+ <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
+ <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+ <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+ </DescentSpeedSchedule>
+ <h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise>
+ <M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise>
+ <AlternateDistance Desc="Reichweite der Alternate Mission" Unit="NM">200</AlternateDistance>
+ <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
+ <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
+ <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
+ <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
+ </StudyMission>
+ <FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod>
+ <V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed>
+ <DesignFlightEnvelope>
+ <VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO>
+ <MMO Desc="Max operating Mach No." Unit="-">0.82</MMO>
+ <h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating>
+ <h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI>
+ </DesignFlightEnvelope>
+ <SizeLimits Desc="maximale geometrische Abmasse">
+ <SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit>
+ </SizeLimits>
+ <ACN Desc="Aircraft Classification Number">
+ <ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType>
+ <ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory>
+ <ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit>
+ </ACN>
+ </Requirements>
+ <DesignSpecification Desc="Spezifikation des Entwurfs">
+ <Configuration Desc="Qualitative Beschreibung der Konfiguration">
+ <Wing Desc="Parameter des Fluegels">
+ <Position Desc="Fluegellage low, mid, high" Unit="-">low</Position>
+ </Wing>
+ <Stabiliser Desc="Parameter des Hoehenleitwerks">
+ <h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing>
+ </Stabiliser>
+ <LandingGear Desc="Fahrwerksanordnung">
+ <MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition>
+ <Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable>
+ <FrictionCoefficient Default="0.03" Desc="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">0.03</FrictionCoefficient>
+ <BrakingCoefficient Default="0.34189" Desc="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">0.34189</BrakingCoefficient>
+ </LandingGear>
+ <Fuselage Desc="Fuselage parameters">
+ <Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized>
+ </Fuselage>
+ <CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType>
+ <Fin Desc="Parameter des Seitenleitwerks">
+ <FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig>
+ </Fin>
+ <SkinThickness Default="0" Desc="Skin thickness of profiles" Unit="m">0</SkinThickness>
+ </Configuration>
+ <Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen">
+ <MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX>
+ <PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks>
+ <PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1">
+ <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes>
+ <Class Desc="Definition der Klasse" ID="1">
+ <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType>
+ <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
+ <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats>
+ </Class>
+ <Class Desc="Definition der Klasse" ID="2">
+ <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType>
+ <Seating Desc="Bestuhlung des Querschnitts">33</Seating>
+ <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats>
+ </Class>
+ <Class Desc="Definition der Klasse" ID="3">
+ <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType>
+ <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
+ <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats>
+ </Class>
+ </PAXDeck>
+ </Accommodation>
+ <Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs">
+ <CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks>
+ <CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1">
+ <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments>
+ <Compartment Desc="Definition des Compartments" ID="1">
+ <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType>
+ <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+ <ULDType Desc="Definition der Containergruppe" ID="1">
+ <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+ <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+ <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs>
+ </ULDType>
+ </Compartment>
+ <Compartment Desc="Definition des Compartments" ID="2">
+ <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType>
+ <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+ <ULDType Desc="Definition der Containergruppe" ID="1">
+ <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+ <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+ <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs>
+ </ULDType>
+ </Compartment>
+ <Compartment Desc="Definition des Compartments" ID="3">
+ <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType>
+ <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+ <ULDType Desc="Definition der Containergruppe" ID="1">
+ <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+ <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+ <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs>
+ </ULDType>
+ </Compartment>
+ </CargoDeck>
+ </Cargo>
+ <Propulsion Desc="Vorgaben zum Antriebssystem">
+ <TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine>
+ <NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines>
+ <PositionOfEngines Desc="Positionierung der Triebwerke">
+ <EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing>
+ <EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage>
+ <EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage>
+ <WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition>
+ </PositionOfEngines>
+ <NumberOfPropulsors Desc="Number of powertrains" ToolLevel="1">2</NumberOfPropulsors>
+ <Propulsor ID="1">
+ <TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
+ <PropulsorPosition>
+ <ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
+ <yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">1</yPosition>
+ <xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
+ </PropulsorPosition>
+ </Propulsor>
+ <Propulsor ID="2">
+ <TypeOfPropulsor Desc="Propulsion technology (Jet or Prop)" Unit="-">Jet</TypeOfPropulsor>
+ <PropulsorPosition>
+ <ParentComponentID Default="MainWing" Desc="ID of the component to which the propulsor is attached (MainWing, Fuselage)">MainWing</ParentComponentID>
+ <yPosition Desc="specific position (0=mid, 1=innerRight, -1=innerLeft, 2=outerRight, -2=outerLeft">-1</yPosition>
+ <xPosition Desc="specific position (0=front, 1=back)">0</xPosition>
+ </PropulsorPosition>
+ </Propulsor>
+ <FuelDensity Desc="Density of fuel" Unit="kg/l">0.785</FuelDensity>
+ </Propulsion>
+ <TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks">
+ <NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks>
+ <NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks>
+ <NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks>
+ </TankConfiguration>
+ <HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem">
+ <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.4</C_LmaxT-O>
+ <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding>
+ </HighLiftSystem>
+ <DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen">
+ <n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1>
+ <n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2>
+ <NormalManeuver Default="1.1" Desc="Normal used load factor for maneuvers (e.g. flare)">1.1</NormalManeuver>
+ </DesignLoads>
+ <Technology Desc="Vorgaben spezieller Technologien">
+ <LaminarFlow Desc="HLFC oder NLF">
+ <Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird">
+ <Wing>
+ <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
+ <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
+ </Wing>
+ <Stabilizer>
+ <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
+ <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
+ </Stabilizer>
+ <Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin>
+ <Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles>
+ </Components>
+ <OperatingCondition>
+ <HLFConlyForCruise>1</HLFConlyForCruise>
+ <MinMachForHLFCActivation>0.78</MinMachForHLFCActivation>
+ </OperatingCondition>
+ </LaminarFlow>
+ <ElectricTaxiing>
+ <DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing>
+ <EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime>
+ </ElectricTaxiing>
+ <BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem>
+ <VariableCamber Desc="Aircraft has VC segments">0</VariableCamber>
+ </Technology>
+ </DesignSpecification>
+</AcftExchangeFile>
diff --git a/scripts/document_aircraft_xml.py b/scripts/document_aircraft_xml.py
new file mode 100644
index 0000000000000000000000000000000000000000..56028039a0d893fa4f49fcdab15d863974394c42
--- /dev/null
+++ b/scripts/document_aircraft_xml.py
@@ -0,0 +1,233 @@
+#!python
+# Copyright (c) 2023 S. Oberschwendtner.
+#
+#
+# This program is free software: you can redistribute it and/or modify
+# it under the terms of the GNU General Public License as published by
+# the Free Software Foundation, either version 3 of the License, or
+# (at your option) any later version.
+#
+# This program is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
+# GNU General Public License for more details.
+#
+# You should have received a copy of the GNU General Public License
+# along with this program. If not, see <https://www.gnu.org/licenses/>.
+
+"""! @brief Script for converting an aircraft XML file to a content page."""
+##
+# @file document_aircraft_xml.py
+#
+# @brief Script for converting an aircraft XML file to a content page for the UNICADO homepage.
+#
+# @section description_document_aircraft_xml Description
+# This script parse the entries of an aircraft XML file and extracts
+# the entries and documents them using their description tags.
+# The output is a markdown file which can be used for the documentation.
+#
+# @section libraries_document_aircraft_xml Libraries/Modules
+# - argparse standard library (https://docs.python.org/3/library/argparse.html)
+# - Parser for command-line options, arguments and sub-commands.
+# - xml standard library (https://docs.python.org/3/library/xml.html)
+# - XML Processing Modules.
+# - pathlib standard library (https://docs.python.org/3/library/pathlib.html)
+# - Object-oriented filesystem paths.
+#
+# @section notes_document_aircraft_xml Notes
+# - None.
+#
+# @section todo_document_aircraft_xml TODO
+# - None.
+#
+# @section authors_document_aircraft_xml Author(s)
+# - Created by S. Oberschwendtner on 19/09/2023.
+
+# === Imports ===
+import argparse
+import xml.etree.ElementTree as ET
+from pathlib import Path
+
+# === Configuration ===
+# Define the format of the output
+FORMAT = {
+ "Header": "# {:s}\n> **Description**: {:s}\n",
+ "Unit": "> **Unit**: {:s}\n",
+ "TableHeader": "| Relative XML Path | Unit | Description |\n|:---|:---:|:---|",
+ "Table": "| <nobr>`{:s}` | *{:s}* | {:s} |",
+}
+
+# Which keys are used in the XML attributes for which information
+KEYS = {
+ "Description": "Desc",
+ "Unit": "Unit",
+}
+
+
+# === Classes ===
+class Page:
+ """Class for a page.
+
+ A page is one top section of the aircraft XML file.
+ """
+
+ @property
+ def max_level_reached(self) -> bool:
+ """Returns whether the maximum level has been reached."""
+ return self.current_level >= self.max_header_level
+
+ def __init__(self, title, max_level):
+ """Constructor of the class.
+
+ Args:
+ title (str): Title of the page.
+ max_level (int): Maximum level of the headers.
+ """
+ self.title = title
+ self.max_header_level = max_level
+ self.current_level = 0
+ self.table_started = False
+ self.current_path = Path(".")
+ self.sections = [[]]
+
+ def create(self, node: ET.Element):
+ """Creates the page from the given node.
+
+ This function adds all subnodes of the given node to the page.
+ It recursively calls itself for all subnodes.
+
+ It does not add sections which are already present in the current level.
+
+ Args:
+ node (ET.Element): Node to start from.
+ """
+ # Only add the header if it was not already added at this level
+ if node.tag in self.sections[self.current_level]:
+ return
+
+ # Check whether the current entry can be a header
+ if not self.max_level_reached:
+ self.sections[self.current_level].append(node.tag)
+ self.make_header_entry(node)
+ self.current_path = Path(node.tag)
+ else:
+ self.current_path /= node.tag
+
+ # Loop through the children and group single entries in a table
+ for child in node:
+ if len(child) == 0:
+ self.make_table_entry(child)
+
+ # Add a new level of sections
+ self.current_level += 1
+ self.sections.append([])
+
+ # Loop again and add the subnodes
+ for child in node:
+ if len(child) > 0:
+ self.create(child)
+
+ # Decrease the level again when finished
+ self.current_level -= 1
+ self.sections.pop()
+ self.current_path = self.current_path.parent
+
+ def make_header_entry(self, node: ET.Element):
+ """Creates a header entry.
+
+ Args:
+ node (ET.Element): The current node element.
+ """
+ # Reset the table when creating a new header
+ self.table_started = False
+
+ # Create the header with description
+ print(
+ "\n"
+ + self.current_level * "#"
+ + FORMAT["Header"].format(
+ node.tag, node.attrib.get(KEYS["Description"], "None")
+ )
+ )
+
+ # Try to add a unit description
+ try:
+ print(FORMAT["Unit"].format(node.attrib[KEYS["Unit"]]))
+ except KeyError:
+ pass
+
+ def make_table_entry(self, node: ET.Element):
+ """Creates a table entry.
+
+ Args:
+ node (ET.Element): The current node element.
+ """
+ # Check if the table has already been started
+ if not self.table_started:
+ self.table_started = True
+ print(FORMAT["TableHeader"])
+
+ # Since we use pathlib for convenience, we need to convert it to a string
+ # and replace the backslashes with forward slashes
+ path_name = str(self.current_path / node.tag).replace("\\", "/")
+
+ # Create the header with description
+ print(
+ FORMAT["Table"].format(
+ path_name,
+ node.attrib.get(KEYS["Unit"], "-"),
+ node.attrib.get(KEYS["Description"], "None"),
+ )
+ )
+
+
+# === Main ===
+def main():
+ """
+ Main function of the script.
+ """
+ # Create argument parser
+ parser = argparse.ArgumentParser(
+ description="Converts an aircraft XML file to a markdown file. The output is streamed to stdout and can be piped to a file."
+ )
+
+ # Add the filename argument
+ parser.add_argument(
+ "filename", metavar="filename", type=str, help="The XML file to convert."
+ )
+
+ # Add the layout arguments
+ parser.add_argument(
+ "--title",
+ metavar="title",
+ type=str,
+ help="The title of the output page. This also sets the root node which is used to create the document.",
+ )
+ parser.add_argument(
+ "--level",
+ metavar="level",
+ type=int,
+ help="The maximum level nodes to be used as headers.",
+ )
+
+ # Parse the arguments
+ args = parser.parse_args()
+
+ # Read the XML file
+ tree = ET.parse(args.filename)
+ root = tree.getroot()
+
+ # Get the configuration parameters
+ page = Page(args.title, args.level)
+ node = root.find(page.title)
+
+ # Check whether the node exists
+ if node is None:
+ raise Warning("Could not find node with title '" + page.title + "'")
+
+ # Start creating the page
+ page.create(node)
+
+
+if __name__ == "__main__":
+ main()