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A320-family/Systems/a320-aerodynamics.xml

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<?xml version="1.0"?>
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<!-- Airbus A320 Aerodynamics -->
<!-- Copyright (c) 2021 Josh Davidson (Octal450) -->
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<aerodynamics> <!-- WIP REWORK 2020 by Josh Davidson (Octal450) -->
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<property value="0">ice/wingL</property>
<property value="0">ice/wingR</property>
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<property value="0">tuneF</property>
<property value="0">tuneS</property>
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<function name="aero/function/kCLge">
<description>Lift factor due to ground effect</description>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.00 1.203
0.10 1.127
0.15 1.090
0.20 1.073
0.30 1.046
0.40 1.055
0.50 1.019
0.60 1.013
0.70 1.008
0.80 1.006
0.90 1.003
1.00 1.002
1.10 1.000
</tableData>
</table>
</function>
<function name="aero/function/kCDge">
<description>Drag factor due to ground effect</description>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.00 0.480
0.10 0.515
0.15 0.629
0.20 0.709
0.30 0.815
0.40 0.882
0.50 0.928
0.60 0.962
0.70 0.988
0.80 1.000
</tableData>
</table>
</function>
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<axis name="LIFT">
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<function name="aero/coefficient/CLalpha">
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<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>aero/function/kCLge</property>
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<table>
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<independentVar lookup="row">aero/alpha-deg</independentVar>
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<tableData>
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-9.8475 -0.5652
-2.0912 0.0625
-0.0098 0.2386
2.2280 0.4260
4.2779 0.5779
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6.4218 0.7540
8.4561 0.9163
9.2699 0.9842
10.7094 1.0843
11.6170 1.1538
12.6496 1.2184
13.7292 1.2811
14.7930 1.3244
15.6981 1.1882
16.6352 1.1064
17.5725 1.0311
18.6045 1.0447
19.6052 1.0479
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30.1264 0.6376
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</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CLq">
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<description>Lift due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>velocities/q-aero-rad_sec</property>
<property>aero/ci2vel</property>
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<value>1.36</value>
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</product>
</function>
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<function name="aero/coefficient/CLadot">
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<description>Lift due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alphadot-rad_sec</property>
<property>aero/ci2vel</property>
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<value>0.6384</value>
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</product>
</function>
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<function name="aero/coefficient/CLflap">
<description>Lift due to flaps</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">fcs/flap-pos-deg</independentVar>
<tableData>
0 0.0000
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10 0.1334
15 0.2314
20 0.3044
40 0.3766
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</tableData>
</table>
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</product>
</function>
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<function name="aero/coefficient/CLslat">
<description>Lift due to slats</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">fcs/slat-pos-deg</independentVar>
<tableData>
0 0.0000
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18 0.2734
22 0.3187
27 0.3523
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</tableData>
</table>
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</product>
</function>
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<function name="aero/coefficient/CLde_l">
<description>Lift due to left elevator</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<toradians><property>hydraulics/elevator-l/final-deg</property></toradians>
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<value>0.0233096</value>
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</product>
</function>
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<function name="aero/coefficient/CLde_r">
<description>Lift due to right elevator</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<toradians><property>hydraulics/elevator-r/final-deg</property></toradians>
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<value>0.0233096</value>
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</product>
</function>
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<function name="aero/coefficient/CLdstab">
<description>Lift due to stabilizer</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>0.0118082</value>
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</product>
</function>
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<function name="aero/coefficient/CLda_l">
<description>Lift due to left aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-l/final-deg</property></toradians>
<value>0.36492</value>
</product>
</function>
<function name="aero/coefficient/CLda_r">
<description>Lift due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-r/final-deg</property></toradians>
<value>0.36492</value>
</product>
</function>
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<function name="aero/coefficient/CLdsp_l">
<description>Lift due to left spoiler</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>-0.0523599</value>
</product>
</function>
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<function name="aero/coefficient/CLdsp_r">
<description>Lift due to right spoiler</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>-0.0523599</value>
</product>
</function>
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<function name="aero/coefficient/CLice_l">
<description>Lift due to left wing ice</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>ice/wingL</independentVar>
<tableData>
0.0 0.00
0.5 -0.05
1.0 -0.15
2.0 -1.25
</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CLice_r">
<description>Lift due to right wing ice</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>ice/wingR</independentVar>
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<tableData>
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0.0 0.00
0.5 -0.05
1.0 -0.15
2.0 -1.25
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</tableData>
</table>
</product>
</function>
</axis>
<axis name="DRAG">
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<function name="aero/coefficient/CD0">
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<description>Minimum drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.0125</value>
</product>
</function>
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<function name="aero/coefficient/CDalpha">
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<description>Drag due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
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<independentVar lookup="row">aero/alpha-deg</independentVar>
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<tableData>
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-14.7960 0.0549
-12.2922 0.0512
-9.4900 0.0379
-6.9768 0.0224
-3.2108 0.0049
0.0000 0.0000
3.2108 0.0049
6.9768 0.0224
9.4900 0.0379
12.2922 0.0512
14.7960 0.0549
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</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CDi">
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<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>aero/function/kCDge</property>
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<property>aero/cl-squared</property>
<value>0.0384</value>
</product>
</function>
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<function name="aero/coefficient/CDmach">
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<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
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0.82 0.000
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1.10 0.016
1.80 0.012
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</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CDbeta">
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<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.23
-0.26 0.05
0.00 0.00
0.26 0.05
1.57 1.23
</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CDgear">
<description>Drag due to gear</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>gear/gear-pos-norm</property>
<value>0.0171</value>
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</product>
</function>
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<function name="aero/coefficient/CDflap">
<description>Drag due to flaps</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
<value>0.00122</value>
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</product>
</function>
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<function name="aero/coefficient/CDslat">
<description>Drag due to slats</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<property>fcs/slat-pos-deg</property>
<value>0.00118</value>
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</product>
</function>
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<function name="aero/coefficient/CDice_l">
<description>Drag due to left wing ice</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<table>
<independentVar>ice/wingL</independentVar>
<tableData>
0.0 0.000
0.5 0.002
1.0 0.005
2.0 0.050
</tableData>
</table>
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</product>
</function>
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<function name="aero/coefficient/CDice_r">
<description>Drag due to right wing ice</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<table>
<independentVar>ice/wingR</independentVar>
<tableData>
0.0 0.000
0.5 0.002
1.0 0.005
2.0 0.050
</tableData>
</table>
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</product>
</function>
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<function name="aero/coefficient/CDde_l">
<description>Drag due to left elevator</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<abs><toradians><property>hydraulics/elevator-l/final-deg</property></toradians></abs>
<value>0.002625</value>
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</product>
</function>
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<function name="aero/coefficient/CDde_r">
<description>Drag due to right elevator</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<abs><toradians><property>hydraulics/elevator-r/final-deg</property></toradians></abs>
<value>0.002625</value>
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</product>
</function>
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<function name="aero/coefficient/CDdstab">
<description>Drag due to stabilizer</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<abs><toradians><property>hydraulics/stabilizer/final-deg</property></toradians></abs>
<value>0.0039</value>
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</product>
</function>
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<function name="aero/coefficient/CDda_l">
<description>Drag due to left aileron</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<abs><toradians><property>hydraulics/aileron-l/final-deg</property></toradians></abs>
<value>0.0029271086286386</value>
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</product>
</function>
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<function name="aero/coefficient/CDda_r">
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<description>Drag due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-r/final-deg</property></toradians></abs>
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<value>0.0029271086286386</value>
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</product>
</function>
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<function name="aero/coefficient/CDdsp_l">
<description>Drag due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>0.025369566928</value>
</product>
</function>
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<function name="aero/coefficient/CDdsp_r">
<description>Drag due to right spoiler</description>
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<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
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<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>0.025369566928</value>
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</product>
</function>
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<function name="aero/coefficient/CDlt_l">
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<description>Drag due to left landing light</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>/controls/lighting/landing-light-pos-l</property>
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<value>0.0016</value>
</product>
</function>
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<function name="aero/coefficient/CDlt_r">
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<description>Drag due to right landing light</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>/controls/lighting/landing-light-pos-r</property>
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<value>0.0016</value>
</product>
</function>
</axis>
<axis name="SIDE">
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<function name="aero/coefficient/CYbeta">
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<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-0.8887</value>
</product>
</function>
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<function name="aero/coefficient/CYp">
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<description>Side force due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<table>
<independentVar lookup="row">aero/Re</independentVar>
<tableData>
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29913298 0.3518
32904628 0.0352
44869948 0.0201
59461352 0.0094
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</tableData>
</table>
</product>
</function>
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<function name="aero/coefficient/CYr">
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<description>Side force due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.8709</value>
</product>
</function>
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<function name="aero/coefficient/CYdr">
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<description>Side force due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
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<value>-0.214</value>
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</product>
</function>
</axis>
<axis name="ROLL">
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<function name="aero/coefficient/Clbeta">
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<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
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<property>aero/beta-deg</property>
<value>0.44</value>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.4412 -0.0034
-2.2116 -0.0038
0.1900 -0.0040
2.4828 -0.0043
4.9473 -0.0043
6.1394 -0.0044
</tableData>
</table>
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</product>
</function>
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<function name="aero/coefficient/Clp">
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<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
2020-11-23 17:54:32 +00:00
<value>-0.58</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Clr">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.1</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Clda_l">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to left aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-l/final-deg</property></toradians>
<value>0.044</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Clda_r">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-r/final-deg</property></toradians>
<value>-0.044</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cldsp_l">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>-0.033</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cldsp_r">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>0.033</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cldr">
2019-10-14 16:48:35 +00:00
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
2020-11-23 17:54:32 +00:00
<value>0.008</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
</axis>
<axis name="PITCH">
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmalpha">
2019-10-14 16:48:35 +00:00
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-9.4468 0.1997
-6.3284 0.1313
-5.4416 0.1101
-4.3131 0.0870
-3.0234 0.0599
-2.0214 0.0359
-0.6629 0.0132
0.4655 -0.0090
1.6628 -0.0281
2.9406 -0.0455
4.0685 -0.0566
5.2651 -0.0624
6.3583 -0.0698
7.3937 -0.0718
8.5212 -0.0736
9.8677 -0.0851
11.3179 -0.1017
20.1549 -0.2027
</tableData>
</table>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmq">
<description>Pitch moment due to pitch rate</description>
2019-10-14 16:48:35 +00:00
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-28.9</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmadot">
<description>Pitch moment due to alpha rate</description>
2019-10-14 16:48:35 +00:00
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-0.94671</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmde_l">
<description>Pitch moment due to left elevator</description>
2019-10-14 16:48:35 +00:00
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<toradians><property>hydraulics/elevator-l/final-deg</property></toradians>
<value>-0.557175</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmde_r">
<description>Pitch moment due to right elevator</description>
2019-10-14 16:48:35 +00:00
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<toradians><property>hydraulics/elevator-r/final-deg</property></toradians>
<value>-0.557175</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cmdstab">
<description>Pitch moment due to stabilizer</description>
2019-10-14 16:48:35 +00:00
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
2020-11-23 17:54:32 +00:00
<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>-1.975</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
</axis>
<axis name="YAW">
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cnbeta">
2019-10-14 16:48:35 +00:00
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
2020-11-23 17:54:32 +00:00
<property>aero/beta-deg</property>
<value>0.44</value>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.7093 0.0045
-2.2164 0.0048
0.2903 0.0044
2.9836 0.0041
5.5629 0.0047
</tableData>
</table>
2019-10-14 16:48:35 +00:00
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cnr">
2019-10-14 16:48:35 +00:00
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.3</value>
</product>
</function>
2020-11-23 17:54:32 +00:00
<function name="aero/coefficient/Cndr">
2019-10-14 16:48:35 +00:00
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
2020-11-23 17:54:32 +00:00
<value>0.061</value>
2019-10-14 16:48:35 +00:00
</product>
</function>
</axis>
</aerodynamics>