/
md-11-aerodynamics.xml
864 lines (783 loc) · 25.4 KB
/
md-11-aerodynamics.xml
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<?xml version="1.0"?>
<!-- McDonnell Douglas MD-11 Aerodynamics -->
<!-- Copyright (c) 2024 Josh Davidson (Octal450) -->
<aerodynamics>
<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>
<axis name="LIFT">
<function name="aero/coefficient/CLalpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData>
0 45000
-9.8475 -0.5652 -0.5935
-2.0912 0.0625 0.0656
-0.0098 0.2386 0.2505
2.2280 0.4260 0.4473
4.2779 0.5779 0.6068
6.4218 0.7540 0.7917
8.4561 0.9163 0.9621
9.2699 0.9842 0.8076
10.7094 1.0843 0.6617
11.6170 1.1538 0.5827
12.6496 1.2184 0.5949
13.7292 1.2911 0.6074
14.7930 1.3444 0.5648
15.6981 1.1882 0.5285
16.6352 1.1064 0.4910
17.5725 1.0311 0.4535
18.6045 1.0447 0.4121
19.6052 1.0479 0.3720
30.1264 0.6376 -0.0494
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLq">
<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>
<value>1.36</value>
</product>
</function>
<function name="aero/coefficient/CLadot">
<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>
<value>0.6384</value>
</product>
</function>
<function name="aero/coefficient/CLflap">
<description>Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">fcs/flap-pos-deg</independentVar>
<tableData>
0 0.0000
15 0.1606
28 0.3312
35 0.4541
50 0.6442
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLslat">
<description>Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<property>fcs/slat-pos-norm</property>
<value>0.1114</value>
</product>
</function>
<function name="aero/coefficient/CLde_lo">
<description>Lift due to left outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/elevator-out-l/final-deg</property></toradians>
<value>0.0116548</value>
</product>
</function>
<function name="aero/coefficient/CLde_li">
<description>Lift due to left inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/elevator-in-l/final-deg</property></toradians>
<value>0.0116548</value>
</product>
</function>
<function name="aero/coefficient/CLde_ri">
<description>Lift due to right inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/elevator-in-r/final-deg</property></toradians>
<value>0.0116548</value>
</product>
</function>
<function name="aero/coefficient/CLde_ro">
<description>Lift due to right outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/elevator-out-r/final-deg</property></toradians>
<value>0.0116548</value>
</product>
</function>
<function name="aero/coefficient/CLdstab">
<description>Lift due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>0.0021645</value>
</product>
</function>
<function name="aero/coefficient/CLda_lo">
<description>Lift due to left outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-out-l/final-deg</property></toradians>
<value>0.018246</value>
</product>
</function>
<function name="aero/coefficient/CLda_li">
<description>Lift due to left inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-in-l/final-deg</property></toradians>
<value>0.018246</value>
</product>
</function>
<function name="aero/coefficient/CLda_ri">
<description>Lift due to right inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-in-r/final-deg</property></toradians>
<value>0.018246</value>
</product>
</function>
<function name="aero/coefficient/CLda_ro">
<description>Lift due to right outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/aileron-out-r/final-deg</property></toradians>
<value>0.018246</value>
</product>
</function>
<function name="aero/coefficient/CLdsp_l">
<description>Lift due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>-0.0261</value>
</product>
</function>
<function name="aero/coefficient/CLdsp_r">
<description>Lift due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>-0.0261</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/coefficient/CD0">
<description>Minimum drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.021</value>
</product>
</function>
<function name="aero/coefficient/CDalpha">
<description>Drag due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-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
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDi">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<property>aero/cl-squared</property>
<value>0.045</value>
</product>
</function>
<function name="aero/coefficient/CDmach">
<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>
0.87 0.000
1.10 0.016
1.80 0.012
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDbeta">
<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>
<function name="aero/coefficient/CDgear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-all-norm</property>
<value>0.0171</value>
</product>
</function>
<function name="aero/coefficient/CDflap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value>0.00132</value>
</product>
</function>
<function name="aero/coefficient/CDslat">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value>0.00128</value>
</product>
</function>
<function name="aero/coefficient/CDde_lo">
<description>Drag due to left outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-out-l/final-deg</property></toradians></abs>
<value>0.003625</value>
</product>
</function>
<function name="aero/coefficient/CDde_li">
<description>Drag due to left inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-in-l/final-deg</property></toradians></abs>
<value>0.003625</value>
</product>
</function>
<function name="aero/coefficient/CDde_ri">
<description>Drag due to right inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-in-r/final-deg</property></toradians></abs>
<value>0.003625</value>
</product>
</function>
<function name="aero/coefficient/CDde_ro">
<description>Drag due to right outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-out-r/final-deg</property></toradians></abs>
<value>0.003625</value>
</product>
</function>
<function name="aero/coefficient/CDdstab">
<description>Drag due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/stabilizer/final-deg</property></toradians></abs>
<value>0.0043</value>
</product>
</function>
<function name="aero/coefficient/CDda_lo">
<description>Drag due to left outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-out-l/final-deg</property></toradians></abs>
<value>0.0023456688</value>
</product>
</function>
<function name="aero/coefficient/CDda_li">
<description>Drag due to left inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-in-l/final-deg</property></toradians></abs>
<value>0.0023456688</value>
</product>
</function>
<function name="aero/coefficient/CDda_ri">
<description>Drag due to right inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-in-r/final-deg</property></toradians></abs>
<value>0.0023456688</value>
</product>
</function>
<function name="aero/coefficient/CDda_ro">
<description>Drag due to right outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-out-r/final-deg</property></toradians></abs>
<value>0.0023456688</value>
</product>
</function>
<function name="aero/coefficient/CDdsp_l">
<description>Drag due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>0.0200716020249513</value>
</product>
</function>
<function name="aero/coefficient/CDdsp_r">
<description>Drag due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>0.0200716020249513</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/coefficient/CYbeta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-0.6093</value>
</product>
</function>
<function name="aero/coefficient/CYp">
<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>
29913298 0.4518
32904628 0.0452
44869948 0.0201
59461352 0.0114
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CYr">
<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>0.6597</value>
</product>
</function>
<function name="aero/coefficient/CYdr_u">
<description>Side force due to upper rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/rudder-upper/final-deg</property></toradians>
<value>-0.08965</value>
</product>
</function>
<function name="aero/coefficient/CYdr_l">
<description>Side force due to lower rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/rudder-lower/final-deg</property></toradians>
<value>-0.08965</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/coefficient/Clbeta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-deg</property>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.4412 -0.00150
-2.2116 -0.00167
0.1900 -0.00176
2.4828 -0.00189
4.9473 -0.00189
6.1394 -0.00194
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Clp">
<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>
<value>-0.61</value>
</product>
</function>
<function name="aero/coefficient/Clr">
<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>
<function name="aero/coefficient/Clda_lo">
<description>Roll moment due to left outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-out-l/final-deg</property></toradians>
<value>0.0184579</value>
</product>
</function>
<function name="aero/coefficient/Clda_li">
<description>Roll moment due to left inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-in-l/final-deg</property></toradians>
<value>0.0314954</value>
</product>
</function>
<function name="aero/coefficient/Clda_ri">
<description>Roll moment due to right inner aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-in-r/final-deg</property></toradians>
<value>-0.0314954</value>
</product>
</function>
<function name="aero/coefficient/Clda_ro">
<description>Roll moment due to right outer aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/aileron-out-r/final-deg</property></toradians>
<value>-0.0184579</value>
</product>
</function>
<function name="aero/coefficient/Cldsp_l">
<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>-0.0155</value>
</product>
</function>
<function name="aero/coefficient/Cldsp_r">
<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>0.0155</value>
</product>
</function>
<function name="aero/coefficient/Cldr_u">
<description>Roll moment due to upper rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder-upper/final-deg</property></toradians>
<value>0.005</value>
</product>
</function>
<function name="aero/coefficient/Cldr_l">
<description>Roll moment due to lower rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder-lower/final-deg</property></toradians>
<value>0.005</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/coefficient/Cmalpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-9.4468 0.2663
-6.3284 0.1750
-5.4416 0.1468
-4.3131 0.1160
-3.0234 0.0799
-2.0214 0.0479
-0.6629 0.0176
0.4655 -0.0120
1.6628 -0.0375
2.9406 -0.0606
4.0685 -0.0755
5.2651 -0.0832
6.3583 -0.0931
7.3937 -0.0957
8.5212 -0.0981
9.8677 -0.1135
11.3179 -0.1356
20.1549 -0.2703
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Cmq">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-31.9</value>
</product>
</function>
<function name="aero/coefficient/Cmadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-12.6734</value>
</product>
</function>
<function name="aero/coefficient/Cmde_lo">
<description>Pitch moment due to left outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/elevator-out-l/final-deg</property></toradians>
<value>-0.16124396</value>
</product>
</function>
<function name="aero/coefficient/Cmde_li">
<description>Pitch moment due to left inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/elevator-in-l/final-deg</property></toradians>
<value>-0.16124396</value>
</product>
</function>
<function name="aero/coefficient/Cmde_ri">
<description>Pitch moment due to right inner elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/elevator-in-r/final-deg</property></toradians>
<value>-0.16124396</value>
</product>
</function>
<function name="aero/coefficient/Cmde_ro">
<description>Pitch moment due to right outer elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/elevator-out-r/final-deg</property></toradians>
<value>-0.16124396</value>
</product>
</function>
<function name="aero/coefficient/Cmdstab">
<description>Pitch moment due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>-2.44152</value>
</product>
</function>
<function name="aero/coefficient/Cmdsp">
<description>Pitch moment due to symmetrical spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0 0.5
1 1.0
</tableData>
</table>
<toradians><property>fcs/spoiler-symmetrical-deg</property></toradians>
<value>0.0125</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/coefficient/Cnbeta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-deg</property>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.7093 0.00198
-2.2164 0.00211
0.2903 0.00194
2.9836 0.00180
5.5629 0.00207
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Cnr">
<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>
<function name="aero/coefficient/Cndr_u">
<description>Yaw moment due to upper rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder-upper/final-deg</property></toradians>
<value>0.015</value>
</product>
</function>
<function name="aero/coefficient/Cndr_l">
<description>Yaw moment due to lower rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder-lower/final-deg</property></toradians>
<value>0.015</value>
</product>
</function>
</axis>
</aerodynamics>