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A-6E_vspaero.xml
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A-6E_vspaero.xml
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<!--
Generated by vsp2jsbsim.py
Author: Jüttner Domokos
Based on the work of Richard Harrison-->
<aerodynamics>
<function name="aero/beta-deg-abs">
<description>Beta absolute value</description>
<abs>
<property>aero/beta-deg</property>
</abs>
</function>
<function name="aero/pb">
<description>PB Denormalization</description>
<product>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
</product>
</function>
<function name="aero/qb">
<description>For denormalization</description>
<product>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
</product>
</function>
<function name="aero/rb">
<description>For denormalization</description>
<product>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
</product>
</function>
<!-- CL -->
<!-- base -->
<function name="aero/CL_base">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.71583 -0.36760 0.00595 0.38606 0.73377 0.84431 0.89900 0.93346 0.96091 0.98057 0.98917 0.99374 0.99472 0.96955
0.60000 -0.77283 -0.41010 0.00613 0.42903 0.79492 0.87702 0.91761 0.94750 0.96681 0.98299 0.99117 0.99862 0.99981 0.93683
0.88000 -0.84859 -0.51310 0.00715 0.52189 0.86891 0.90895 0.93031 0.95352 0.97415 0.99899 1.00372 1.01955 1.00451 0.98946
0.92000 -0.85815 -0.54662 0.00762 0.55472 0.87760 0.91176 0.93057 0.95115 0.98030 1.00556 1.01844 1.03335 1.02926 1.00005
0.96000 -0.86451 -0.59772 0.00831 0.59677 0.88294 0.91665 0.94335 0.96578 0.98888 1.02061 1.04864 1.06712 1.05768 1.02736
0.98000 -0.86816 -0.63411 0.00881 0.63314 0.89412 0.92249 0.95097 0.96844 0.99862 1.05222 1.08370 1.10532 1.10463 1.07030
1.01000 -0.86120 -0.76259 -0.00458 0.75284 0.84431 0.85757 0.87369 0.89057 0.90984 0.94681 0.97359 0.96804 0.95790 0.93667
</tableData>
<tableData breakPoint="-5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.73951 -0.37767 0.00636 0.38745 0.74972 0.85741 0.90126 0.93538 0.96433 0.99110 0.99528 1.00035 1.00645 0.99905
0.60000 -0.79484 -0.42084 0.00665 0.43769 0.80527 0.88450 0.91407 0.94461 0.96912 0.99636 0.99523 1.00521 1.00968 1.01058
0.88000 -0.85563 -0.52579 0.00767 0.52946 0.87763 0.90611 0.92690 0.96767 0.98865 0.99948 1.00446 1.02376 1.02549 1.01516
0.92000 -0.86367 -0.56045 0.00802 0.53442 0.88580 0.88786 0.94908 0.96702 0.98817 1.00226 1.01751 1.03804 1.04291 1.03018
0.96000 -0.86941 -0.61412 0.00849 0.62639 0.86957 0.92943 0.95251 0.96192 0.99222 1.01329 1.03222 1.07373 1.07705 1.06196
0.98000 -0.87319 -0.65693 0.00881 0.61511 0.90963 0.92465 0.95796 0.97529 1.00246 1.03445 1.08231 1.11919 1.12784 1.10674
1.01000 -0.86529 -0.77638 -0.00539 0.75864 0.84939 0.85662 0.88096 0.89516 0.91123 0.95655 0.97745 0.97565 0.97295 0.96705
</tableData>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.74905 -0.38086 0.00633 0.39095 0.76497 0.86487 0.91225 0.94461 0.96771 0.98873 0.99444 1.00358 1.01166 1.00898
0.60000 -0.80118 -0.42427 0.00672 0.43455 0.81541 0.89247 0.93028 0.95668 0.97495 0.99250 0.99812 1.00797 1.01531 1.01941
0.88000 -0.85699 -0.53041 0.00782 0.53950 0.88224 0.92475 0.94608 0.96378 0.98792 1.00630 1.01406 1.02639 1.03317 1.02703
0.92000 -0.86428 -0.56514 0.00814 0.57338 0.89268 0.92577 0.94816 0.96675 0.99298 1.01488 1.02429 1.04058 1.04814 1.04156
0.96000 -0.86977 -0.61934 0.00857 0.62378 0.89951 0.92805 0.95449 0.97335 1.00098 1.03710 1.05280 1.07740 1.08459 1.07480
0.98000 -0.87327 -0.66455 0.00883 0.66054 0.90651 0.93798 0.96287 0.98143 1.01295 1.06740 1.09323 1.12459 1.13576 1.11974
1.01000 -0.86673 -0.78169 -0.00566 0.76508 0.85119 0.86654 0.88290 0.90073 0.92063 0.96549 0.97831 0.97827 0.97818 0.97799
</tableData>
<tableData breakPoint="5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.73972 -0.37771 0.00632 0.38706 0.74933 0.85740 0.90111 0.93476 0.96405 0.99099 0.99524 1.00027 1.00648 1.00122
0.60000 -0.79489 -0.42084 0.00663 0.43182 0.80503 0.88439 0.91384 0.94407 0.96760 0.99632 0.99500 1.00518 1.00963 1.01056
0.88000 -0.85566 -0.52582 0.00766 0.53365 0.87859 0.90554 0.92717 0.96771 0.98862 1.00023 1.00442 1.02381 1.02467 1.01509
0.92000 -0.86370 -0.56070 0.00801 0.55985 0.88530 0.88854 0.94933 0.96681 0.98819 1.00242 1.01738 1.03821 1.04291 1.03006
0.96000 -0.86945 -0.61417 0.00848 0.62736 0.86948 0.92988 0.95254 0.96223 0.99241 1.01341 1.03325 1.07560 1.07707 1.06199
0.98000 -0.87321 -0.65692 0.00880 0.61415 0.90950 0.92475 0.95812 0.97575 1.00273 1.03502 1.08268 1.11896 1.12802 1.10703
1.01000 -0.86523 -0.77637 -0.00538 0.75863 0.84936 0.85684 0.88100 0.89510 0.91089 0.95785 0.97745 0.97565 0.97295 0.96706
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.71605 -0.36763 0.00588 0.38742 0.73387 0.84449 0.89915 0.93375 0.96080 0.98034 0.98949 0.99368 0.99460 0.97046
0.60000 -0.77297 -0.41013 0.00607 0.42920 0.79520 0.87702 0.91777 0.94757 0.96677 0.98295 0.99146 0.99854 0.99994 0.93561
0.88000 -0.84872 -0.51313 0.00710 0.52203 0.86855 0.90874 0.93023 0.95337 0.97423 0.99904 1.00377 1.01978 1.00447 0.98936
0.92000 -0.85825 -0.54666 0.00760 0.55459 0.87746 0.91159 0.93023 0.94946 0.98075 1.00590 1.01803 1.03652 1.02919 0.99996
0.96000 -0.86453 -0.59782 0.00831 0.59724 0.88292 0.91659 0.94317 0.96560 0.98864 1.02097 1.04887 1.06699 1.05768 1.02739
0.98000 -0.86820 -0.63411 0.00881 0.63345 0.89438 0.92240 0.95079 0.96837 0.99892 1.05326 1.08264 1.10521 1.10485 1.07028
1.01000 -0.86116 -0.76258 -0.00457 0.75283 0.84428 0.85740 0.87369 0.89059 0.91022 0.94686 0.97362 0.96804 0.95791 0.93667
</tableData>
</table>
</function>
<!-- elevator -->
<function name="aero/CL_elevator_-24">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.11328 -0.16331 -0.20544 -0.24554 -0.28856 -0.28947 -0.29987 -0.30957 -0.31350 -0.28869 -0.24114 -0.13518 -0.03814 -0.00369
0.60000 -0.09842 -0.15743 -0.20128 -0.24235 -0.27305 -0.29026 -0.30489 -0.31832 -0.32891 -0.31116 -0.26266 -0.15172 -0.04569 -0.00032
0.88000 -0.08798 -0.14538 -0.19031 -0.23023 -0.26657 -0.28828 -0.30779 -0.32311 -0.34356 -0.34943 -0.33076 -0.21095 -0.07814 0.00052
0.92000 -0.08718 -0.14273 -0.18685 -0.22506 -0.26580 -0.28533 -0.30590 -0.32019 -0.34141 -0.35340 -0.34615 -0.23592 -0.09398 0.00087
0.96000 -0.08985 -0.13950 -0.18200 -0.21702 -0.26227 -0.28060 -0.30064 -0.31224 -0.33251 -0.35317 -0.35252 -0.27819 -0.12260 0.00094
0.98000 -0.09320 -0.13787 -0.17868 -0.20863 -0.25808 -0.27889 -0.29345 -0.30160 -0.32144 -0.35137 -0.35389 -0.31519 -0.15130 -0.00018
1.01000 -0.11162 -0.14624 -0.17511 -0.19355 -0.22809 -0.24344 -0.25980 -0.27764 -0.29754 -0.34241 -0.35524 -0.35525 -0.22701 0.00000
</tableData>
</table>
</function>
<function name="aero/CL_elevator_-9.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.10010 -0.13259 -0.13693 -0.14023 -0.13807 -0.13322 -0.12909 -0.12481 -0.11839 -0.09460 -0.05248 -0.00665 -0.00049 -0.00429
0.60000 -0.09250 -0.13688 -0.14690 -0.15068 -0.14406 -0.14344 -0.14034 -0.13689 -0.13073 -0.10125 -0.05593 -0.00469 0.00000 0.00000
0.88000 -0.08668 -0.13656 -0.16779 -0.17387 -0.17072 -0.17122 -0.16915 -0.16373 -0.16529 -0.12715 -0.07572 -0.00249 0.00025 0.00076
0.92000 -0.08697 -0.13597 -0.17100 -0.18097 -0.18038 -0.18174 -0.17867 -0.17282 -0.17589 -0.14004 -0.08695 -0.00288 0.00042 0.00027
0.96000 -0.09003 -0.13554 -0.17320 -0.18816 -0.19324 -0.19589 -0.19302 -0.18687 -0.19203 -0.16533 -0.10918 -0.00380 0.00069 0.00023
0.98000 -0.09370 -0.13601 -0.17420 -0.19100 -0.20468 -0.21223 -0.20510 -0.19829 -0.20529 -0.18874 -0.13185 -0.00544 0.00086 0.00011
1.01000 -0.10439 -0.14634 -0.17511 -0.19237 -0.21777 -0.22761 -0.23756 -0.24269 -0.24268 -0.23946 -0.19190 -0.03813 0.00000 0.00000
</tableData>
</table>
</function>
<function name="aero/CL_elevator_-3">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.04073 -0.04318 -0.04448 -0.03522 -0.04304 -0.04157 -0.03928 -0.03738 -0.03547 -0.01522 -0.00033 -0.00022 -0.00086 -0.00041
0.60000 -0.04304 -0.04696 -0.04801 -0.04937 -0.04539 -0.04470 -0.04302 -0.04119 -0.03942 -0.01287 -0.00010 -0.00014 -0.00050 0.00017
0.88000 -0.05066 -0.05295 -0.05554 -0.05811 -0.05431 -0.05404 -0.05256 -0.04653 -0.04925 -0.01450 0.00017 0.00000 0.00000 -0.00025
0.92000 -0.05308 -0.05606 -0.05776 -0.06088 -0.05745 -0.05717 -0.05570 -0.04886 -0.05255 -0.01928 0.00013 0.00013 0.00000 0.00000
0.96000 -0.05739 -0.05920 -0.06100 -0.06494 -0.06172 -0.06144 -0.06067 -0.05193 -0.05697 -0.03251 -0.00199 -0.00028 0.00017 0.00014
0.98000 -0.06055 -0.06131 -0.06353 -0.07253 -0.06542 -0.06895 -0.06477 -0.06380 -0.06074 -0.04552 -0.00632 0.00118 -0.00327 -0.00018
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</tableData>
</table>
</function>
<function name="aero/CL_elevator_1.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.02061 0.02151 0.02207 0.02185 0.02058 0.01963 0.01863 0.01762 0.01276 0.00111 0.00000 0.00000 -0.00086 -0.00040
0.60000 0.02172 0.02253 0.02380 0.02363 0.02180 0.02176 0.02018 0.01884 0.00971 0.00000 0.00013 0.00000 -0.00076 0.00000
0.88000 0.02599 0.02602 0.02749 0.02820 0.02574 0.02701 0.02474 0.02225 0.00902 -0.00013 0.00000 0.00035 -0.00030 -0.00033
0.92000 0.02734 0.02699 0.02857 0.02990 0.02653 0.02855 0.02610 0.02375 0.01038 0.00000 -0.00055 0.00059 -0.00023 0.00000
0.96000 0.02916 0.02813 0.03012 0.03155 0.02967 0.03184 0.02855 0.02755 0.01670 -0.00073 0.00000 0.00030 0.00000 0.00000
0.98000 0.03069 0.02888 0.03133 0.04028 0.02905 0.03111 0.03049 0.02979 0.02388 -0.00118 0.00035 0.00063 -0.00010 -0.00014
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</tableData>
</table>
</function>
<function name="aero/CL_elevator">
<interpolate1d>
<property>fcs/surfaces/elevator-pos-deg</property>
<value>-24</value> <property>aero/CL_elevator_-24</property>
<value>-9.5</value> <property>aero/CL_elevator_-9.5</property>
<value>-3</value> <property>aero/CL_elevator_-3</property>
<value>0</value> <value>0</value>
<value>1.5</value> <property>aero/CL_elevator_1.5</property>
</interpolate1d>
</function>
<!-- flaps -->
<function name="aero/CL_flaps_20">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.41879 0.42734 0.42539 0.39932 0.38630 0.40832 0.46811 0.49140 0.50503 0.55035 0.59977 0.64170 0.60100 0.40138
0.60000 0.44470 0.48720 0.48325 0.45170 0.44659 0.45095 0.47823 0.52467 0.53566 0.58007 0.62520 0.67370 0.64971 0.48420
0.88000 0.45819 0.65516 0.65210 0.60842 0.49189 0.48922 0.57641 0.57939 0.57558 0.61022 0.65330 0.71655 0.72538 0.62963
0.92000 0.46026 0.71893 0.71563 0.56152 0.47827 0.55719 0.58052 0.58725 0.58053 0.61345 0.65495 0.72579 0.73951 0.66398
0.96000 0.46809 0.82878 0.85199 0.65788 0.58408 0.59039 0.59601 0.60303 0.59015 0.60749 0.65420 0.74092 0.75357 0.69499
0.98000 0.48593 0.93124 0.92343 0.48335 0.60672 0.60752 0.61191 0.59671 0.59670 0.61081 0.65540 0.75669 0.76524 0.70774
1.01000 0.21428 0.96427 0.96756 0.48396 0.64591 0.62524 0.60802 0.59426 0.58406 0.57243 0.60763 0.72288 0.73389 0.73387
</tableData>
</table>
</function>
<function name="aero/CL_flaps_30">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
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0.60000 0.62640 0.66602 0.65311 0.61702 0.50561 0.47545 0.48178 0.52315 0.54737 0.57829 0.62296 0.67326 0.65200 0.48651
0.88000 0.70174 0.89483 0.88072 0.63162 0.51977 0.48977 0.51687 0.59488 0.57394 0.59706 0.64807 0.71489 0.72786 0.63107
0.92000 0.72743 0.98176 0.96586 0.61565 0.50579 0.50694 0.60043 0.59037 0.57369 0.60782 0.65077 0.72406 0.74059 0.66430
0.96000 0.77777 1.12930 1.07767 0.51253 0.56998 0.61551 0.60490 0.60351 0.58749 0.60677 0.65303 0.74388 0.75783 0.69793
0.98000 0.83264 1.26924 1.10555 0.86559 0.64301 0.63427 0.62177 0.59701 0.59745 0.61065 0.65954 0.76209 0.77243 0.71166
1.01000 0.60141 1.33097 1.12489 0.48648 0.66696 0.63665 0.61222 0.59343 0.57915 0.56349 0.59809 0.71942 0.73391 0.73390
</tableData>
</table>
</function>
<function name="aero/CL_flaps">
<interpolate1d>
<property>fcs/surfaces/flaps-pos-deg</property>
<value>0</value> <value>0</value>
<value>20</value> <property>aero/CL_flaps_20</property>
<value>30</value> <property>aero/CL_flaps_30</property>
</interpolate1d>
</function>
<!-- left-flaperon -->
<function name="aero/CL_left-flaperon_-51">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.04378 -0.14848 -0.16607 -0.16128 -0.19002 -0.11985 -0.05671 -0.00133 0.00359 -0.00151 -0.03754 -0.00400 -0.00143 -0.00361
0.60000 -0.02582 -0.15133 -0.19107 -0.18787 -0.16740 -0.10063 -0.02652 0.00617 -0.00203 0.00245 -0.03559 -0.00553 -0.00221 -0.00312
0.88000 -0.01186 -0.14502 -0.25715 -0.23921 -0.18422 -0.06322 -0.00253 -0.01974 0.01146 -0.04268 -0.01551 -0.02131 -0.00617 -0.00437
0.92000 -0.01006 -0.13727 -0.28017 -0.20683 -0.14936 -0.07629 0.02638 0.00592 -0.08308 -0.02318 -0.02268 -0.00840 -0.00697 -0.01329
0.96000 -0.00052 -0.04138 -0.14188 -0.33382 -0.14480 -0.08297 -0.01377 -0.01608 -0.05057 -0.01613 -0.03349 -0.02880 -0.01197 -0.03185
0.98000 0.26469 0.17600 -0.24087 -0.38233 -0.14929 -0.09106 0.01510 0.02182 0.00871 -0.01823 -0.05031 -0.07798 -0.02056 -0.02318
1.01000 -0.01128 -0.00978 -0.21127 -0.24653 -0.03625 -0.04192 -0.02935 -0.04022 -0.04162 -0.14078 -0.09826 -0.04850 -0.01951 -0.00125
</tableData>
</table>
</function>
<function name="aero/CL_left-flaperon">
<interpolate1d>
<property>fcs/surfaces/left-flaperon-pos-deg</property>
<value>-51</value> <property>aero/CL_left-flaperon_-51</property>
<value>0</value> <value>0</value>
</interpolate1d>
</function>
<!-- right-flaperon -->
<function name="aero/CL_right-flaperon_-51">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
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0.60000 -0.02583 -0.15152 -0.19012 -0.20540 -0.16826 -0.10114 -0.02661 0.00543 -0.00128 0.00283 -0.03798 -0.00569 -0.00230 -0.00326
0.88000 -0.01179 -0.14499 -0.25716 -0.23954 -0.15450 -0.06201 -0.00244 -0.01959 0.01134 -0.04461 -0.01579 -0.02132 -0.00633 -0.00447
0.92000 -0.01002 -0.13711 -0.28019 -0.22307 -0.14505 -0.07615 0.01367 0.00545 -0.08285 -0.02377 -0.02047 -0.00493 -0.00732 -0.01099
0.96000 -0.00035 -0.04146 -0.16154 -0.36413 -0.14663 -0.08304 -0.01364 -0.01367 -0.05061 -0.01557 -0.03380 -0.02978 -0.01207 -0.03196
0.98000 0.26642 0.17483 -0.24270 -0.32777 -0.14988 -0.09486 0.01511 0.02348 0.00846 -0.01829 -0.05038 -0.07671 -0.02013 -0.02337
1.01000 -0.01128 -0.00976 -0.21129 -0.24476 -0.03626 -0.04200 -0.02977 -0.04020 -0.04160 -0.14087 -0.09900 -0.04863 -0.01944 -0.00111
</tableData>
</table>
</function>
<function name="aero/CL_right-flaperon">
<interpolate1d>
<property>fcs/surfaces/right-flaperon-pos-deg</property>
<value>-51</value> <property>aero/CL_right-flaperon_-51</property>
<value>0</value> <value>0</value>
</interpolate1d>
</function>
<!-- rudder -->
<function name="aero/CL_rudder_-35">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00497 0.00577 0.00460 0.00719 -0.00106 -0.00038 0.00337 0.00736 0.01272 -0.00238 -0.08562 -0.02446 -0.00989 0.00267
0.60000 0.00795 0.00925 0.00943 0.01264 -0.00263 -0.00505 0.00509 0.00876 0.01045 -0.07538 -0.08658 -0.02386 -0.00639 0.01154
0.88000 0.03282 0.04210 0.04856 0.04698 0.01604 0.02119 0.04860 -0.00511 -0.01639 -0.04716 -0.01496 -0.02353 -0.00163 -0.00596
0.92000 0.06342 0.06946 0.08304 0.07410 0.04306 0.02673 0.08241 -0.00980 -0.04344 -0.06562 -0.00952 -0.02208 -0.00563 -0.00443
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0.98000 0.33336 0.25410 0.14918 0.17023 0.11235 0.05671 0.05709 0.18021 0.02430 -0.13323 -0.02072 -0.02842 -0.00797 -0.00447
1.01000 0.16368 0.15519 0.13407 0.12350 0.10822 0.10116 0.08662 0.07441 0.05378 -0.04842 -0.10450 -0.11068 -0.10176 -0.06001
</tableData>
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-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00228 0.00178 0.00164 0.01340 -0.00279 -0.00513 -0.00532 0.00600 0.00789 -0.01108 -0.02067 0.00526 -0.00489 -0.00068
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0.98000 0.21449 0.16789 0.07590 0.50970 -0.00847 0.03300 0.02287 0.01762 -0.03295 -0.02807 0.00407 -0.04432 -0.01080 -0.00913
1.01000 0.06274 0.06675 0.07011 0.13219 0.06551 0.01707 -0.02169 -0.02271 -0.03254 -0.04784 -0.10911 -0.11051 -0.03425 -0.01361
</tableData>
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-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00243 0.00077 0.00045 -0.06236 -0.00756 0.00000 0.00369 0.00071 -0.00175 -0.00893 -0.10075 -0.00644 -0.00320 -0.00329
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1.01000 0.00848 0.00609 0.00351 0.00058 -0.00202 -0.00354 -0.00492 -0.00622 -0.00764 -0.00988 -0.01147 -0.01344 -0.01328 -0.01065
</tableData>
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0.20000 0.00339 0.00505 -0.00427 0.00384 -0.00909 0.02248 0.02278 0.00660 -0.00502 -0.01330 0.00721 -0.02687 -0.01825 0.00000
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0.88000 0.01471 0.02561 0.04610 3.30544 -0.05739 0.03999 0.02323 -0.00701 0.00411 -0.07041 -0.03429 -0.03417 -0.00112 -0.00291
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1.01000 0.07109 0.07624 0.07741 0.12644 0.05833 0.00932 -0.02941 -0.01597 -0.02979 -0.04808 -0.11483 -0.09931 -0.03587 -0.00662
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00839 0.01731 0.05900 0.05130 0.01280 0.00611 0.02920 0.02366 -0.01513 -0.04495 -0.09954 0.04725 -0.02192 0.00638
0.60000 0.01270 0.02215 0.05164 0.02453 0.01241 0.00623 0.02454 -0.00194 -0.04029 -0.06492 -0.07087 -0.02084 -0.00820 0.02276
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0.98000 1.41297 0.09187 0.14933 0.16869 0.09002 0.05524 0.04340 0.02748 0.06573 -0.04722 -0.04020 -0.02142 -0.00432 -0.00324
1.01000 0.17148 0.16163 0.13777 0.12327 0.10561 0.09831 0.08625 0.07834 0.05371 -0.06078 -0.10884 -0.10199 -0.09896 -0.05320
</tableData>
</table>
</function>
<function name="aero/CL_rudder_35">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00883 0.01725 0.05684 0.05054 0.01258 0.00610 0.03032 0.02480 -0.01347 -0.04611 -0.09938 0.04756 -0.02192 0.00726
0.60000 0.01314 0.02218 0.05004 0.01884 0.01261 0.00692 0.02427 -0.00196 -0.04135 -0.06682 -0.07066 -0.02045 -0.00849 0.02327
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1.01000 0.17160 0.16162 0.13771 0.12344 0.10533 0.09787 0.08631 0.07853 0.05400 -0.06066 -0.10876 -0.10200 -0.09896 -0.05312
</tableData>
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0.20000 0.00371 0.00504 0.00367 -0.00557 -0.00924 0.02358 0.02303 0.00585 -0.00565 -0.01294 0.00936 -0.02700 -0.01955 0.00173
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0.92000 0.00412 0.00259 0.00251 -0.00724 0.00253 -0.00322 -0.00155 -0.00244 -0.07648 -0.00589 -0.00671 -0.00680 -0.00752 -0.00817
0.96000 0.00481 0.00375 0.01793 -0.00522 -0.00223 -0.00247 -0.00234 0.04752 -0.00366 -0.00682 -0.00916 -0.00991 -0.00807 -0.00853
0.98000 0.12861 0.00455 0.00376 -0.01410 -0.00125 -0.05901 -0.01825 -0.00159 -0.00330 -0.00668 -0.00795 -0.01114 -0.00996 -0.00797
1.01000 0.00848 0.00610 0.00352 0.00068 -0.00204 -0.00354 -0.00492 -0.00618 -0.00768 -0.00981 -0.01145 -0.01344 -0.01329 -0.01067
</tableData>
<tableData breakPoint="5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00240 0.00189 0.00166 0.01131 -0.00284 -0.00521 -0.00636 0.00657 0.00805 -0.01047 -0.01955 0.00419 -0.00500 -0.00280
0.60000 0.00329 0.00329 0.00396 0.01575 -0.00163 -0.01807 0.00119 0.02745 0.02340 -0.01573 -0.05330 -0.01015 -0.00344 -0.00337
0.88000 0.01013 0.01290 0.04107 0.08587 -0.03944 -0.03227 0.01993 0.00581 -0.06288 -0.05274 -0.03551 -0.01293 -0.00353 -0.00576
0.92000 0.01836 0.02851 0.14634 0.10045 -0.03170 0.01838 0.00909 0.00787 -0.00597 -0.02136 -0.03439 -0.01624 -0.00708 -0.00585
0.96000 0.08482 0.16804 0.09011 0.11811 0.07514 -0.01765 0.03396 0.05413 0.00632 -0.02238 -0.00633 -0.03180 -0.00983 -0.00722
0.98000 0.21278 0.16823 0.07532 0.30259 -0.00857 0.03262 0.02234 0.01748 -0.03378 -0.02859 0.00426 -0.04575 -0.01112 -0.01002
1.01000 0.06264 0.06673 0.07011 0.13207 0.06601 0.01606 -0.02178 -0.02280 -0.03218 -0.04917 -0.10913 -0.11052 -0.03431 -0.01364
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00466 0.00572 0.00505 0.00533 -0.00212 -0.00045 0.00290 0.00727 0.01314 -0.00186 -0.08591 -0.02461 -0.00939 0.00129
0.60000 0.00759 0.00923 0.01011 0.01269 -0.00264 -0.00502 0.00571 0.01008 0.01006 -0.07943 -0.08605 -0.02379 -0.00607 0.01043
0.88000 0.03310 0.04238 0.04908 0.04701 0.01638 0.02296 0.04939 -0.00488 -0.01520 -0.04971 -0.01573 -0.02226 -0.00230 -0.00607
0.92000 0.06365 0.06951 0.08316 0.07503 0.04190 0.02615 0.08384 -0.02692 -0.04182 -0.06673 -0.00927 -0.02518 -0.00690 -0.00587
0.96000 0.15722 0.16253 0.21788 0.07273 0.02988 0.04877 0.02684 -0.02948 -0.03347 -0.05056 0.27577 -0.02858 -0.00730 -0.00350
0.98000 0.33385 0.25021 0.14917 0.16942 0.11355 0.05789 0.05100 0.26996 0.02538 -0.13777 -0.01599 -0.02821 -0.00811 -0.00597
1.01000 0.16356 0.15523 0.13413 0.12353 0.10850 0.10146 0.08641 0.07429 0.05345 -0.04847 -0.10454 -0.11070 -0.10174 -0.06013
</tableData>
</table>
</function>
<function name="aero/CL_rudder">
<interpolate1d>
<property>fcs/surfaces/rudder-pos-deg</property>
<value>-35</value> <property>aero/CL_rudder_-35</property>
<value>0</value> <value>0</value>
<value>35</value> <property>aero/CL_rudder_35</property>
</interpolate1d>
</function>
<!-- slats -->
<function name="aero/CL_slats_27.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.00097 -0.00958 -0.01502 -0.01273 -0.00754 0.08139 0.19202 0.24951 0.28390 0.33835 0.37848 0.40909 0.38819 0.26718
0.60000 -0.03221 -0.00966 -0.01598 -0.01462 0.02435 0.15994 0.24335 0.28624 0.31286 0.36047 0.39984 0.41847 0.40885 0.31896
0.88000 -0.17713 -0.00892 -0.01676 -0.01720 0.16935 0.26884 0.31486 0.33485 0.34850 0.37770 0.40918 0.42212 0.42009 0.39226
0.92000 -0.21890 -0.00810 -0.01635 -0.02365 0.21422 0.29260 0.32734 0.34287 0.34800 0.37673 0.40963 0.42225 0.42104 0.39793
0.96000 -0.26638 -0.00605 -0.01483 -0.05551 0.26034 0.31855 0.33771 0.34911 0.34875 0.36963 0.40792 0.42223 0.42142 0.40125
0.98000 -0.28543 -0.00338 -0.01250 -0.09230 0.28616 0.32489 0.34446 0.34956 0.34891 0.36155 0.40377 0.42231 0.42061 0.40083
1.01000 -0.34161 -0.06271 -0.00631 0.05112 0.35137 0.35471 0.35394 0.35318 0.35228 0.35102 0.38868 0.42396 0.42210 0.41840
</tableData>
</table>
</function>
<function name="aero/CL_slats">
<interpolate1d>
<property>fcs/surfaces/slats-pos-deg</property>
<value>0</value> <value>0</value>
<value>27.5</value> <property>aero/CL_slats_27.5</property>
</interpolate1d>
</function>
<!-- CDTOT -->
<!-- base -->
<function name="aero/CDtot_base">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.06412 0.03608 0.02620 0.03979 0.06068 0.07930 0.09518 0.11113 0.12460 0.14832 0.19506 0.28591 0.44125 0.73125
0.60000 0.07170 0.03841 0.02649 0.04379 0.06929 0.08636 0.10406 0.12144 0.13703 0.16214 0.21490 0.32091 0.50472 0.85478
0.88000 0.08773 0.04473 0.02698 0.05296 0.08782 0.10209 0.12309 0.14264 0.16172 0.19497 0.26044 0.39777 0.63586 1.11320
0.92000 0.09194 0.04704 0.02708 0.05687 0.09331 0.10838 0.12886 0.15721 0.16944 0.20567 0.27573 0.41795 0.66227 1.15181
0.96000 0.09778 0.05073 0.02717 0.06307 0.10116 0.11625 0.13730 0.16010 0.18212 0.22137 0.29719 0.44687 0.68710 1.14505
0.98000 0.10251 0.05396 0.02720 0.06949 0.10745 0.12130 0.14438 0.17211 0.19267 0.23301 0.31760 0.47587 0.70028 1.07555
1.01000 0.18445 0.10076 0.03215 0.10258 0.18413 0.23367 0.26851 0.31635 0.36593 0.47631 0.59205 0.83501 1.15726 1.62990
</tableData>
<tableData breakPoint="-5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.06252 0.03352 0.02341 0.03430 0.06291 0.07876 0.09335 0.10852 0.12227 0.15613 0.19091 0.28384 0.43841 0.73611
0.60000 0.07002 0.03585 0.02348 0.03732 0.07077 0.08597 0.10056 0.11856 0.13263 0.17077 0.21008 0.31783 0.50057 0.85899
0.88000 0.08437 0.04255 0.02360 0.04371 0.08556 0.10070 0.11829 0.13935 0.17413 0.20255 0.25026 0.38556 0.62085 1.10343
0.92000 0.08815 0.04508 0.02363 0.04720 0.08975 0.10464 0.12345 0.14510 0.18924 0.21255 0.26168 0.40063 0.63885 1.12953
0.96000 0.09321 0.04932 0.02365 0.05144 0.09419 0.11117 0.13233 0.15111 0.21480 0.22440 0.27567 0.41192 0.63384 1.08127
0.98000 0.09714 0.05314 0.02367 0.05573 0.09771 0.11657 0.14569 0.15139 0.17340 0.22930 0.28503 0.41045 0.59573 0.94398
1.01000 0.18099 0.09632 0.02497 0.09551 0.17853 0.24775 0.26408 0.31960 0.39060 0.49632 0.59199 0.84425 1.18252 1.69441
</tableData>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.06201 0.03267 0.02251 0.03322 0.06157 0.07823 0.09268 0.10702 0.12194 0.15373 0.18834 0.28180 0.43756 0.74161
0.60000 0.06931 0.03501 0.02251 0.03558 0.06888 0.08532 0.10043 0.11620 0.13282 0.16787 0.20719 0.31547 0.49935 0.86481
0.88000 0.08304 0.04186 0.02251 0.04210 0.08259 0.09919 0.11674 0.13461 0.15571 0.19788 0.24602 0.38077 0.61588 1.10427
0.92000 0.08663 0.04447 0.02251 0.04445 0.08596 0.10292 0.12120 0.13967 0.16175 0.20622 0.25612 0.39365 0.63055 1.12509
0.96000 0.09128 0.04893 0.02251 0.04819 0.09017 0.10778 0.12700 0.14597 0.16892 0.21696 0.26726 0.39806 0.61412 1.06110
0.98000 0.09458 0.05306 0.02251 0.05133 0.09283 0.11158 0.13044 0.14921 0.17238 0.22189 0.26952 0.38197 0.55676 0.90028
1.01000 0.17979 0.09480 0.02250 0.09335 0.17696 0.21897 0.26340 0.31078 0.36192 0.47715 0.59169 0.84713 1.19132 1.71785
</tableData>
<tableData breakPoint="5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.06254 0.03352 0.02341 0.03433 0.06285 0.07875 0.09338 0.10851 0.12238 0.15615 0.19090 0.28384 0.43846 0.73620
0.60000 0.07002 0.03585 0.02348 0.03697 0.07077 0.08595 0.10105 0.11853 0.13225 0.17082 0.21005 0.31786 0.50062 0.85907
0.88000 0.08437 0.04255 0.02360 0.04398 0.08569 0.10068 0.11826 0.13932 0.17390 0.20268 0.25019 0.38550 0.62055 1.10321
0.92000 0.08815 0.04509 0.02363 0.04640 0.08972 0.10456 0.12345 0.14508 0.18925 0.21256 0.26158 0.40052 0.63874 1.12938
0.96000 0.09322 0.04933 0.02365 0.05137 0.09435 0.11131 0.13232 0.15107 0.21528 0.22434 0.27552 0.41203 0.63373 1.08095
0.98000 0.09713 0.05314 0.02367 0.05576 0.09777 0.11663 0.14573 0.15139 0.17308 0.22922 0.28485 0.41019 0.59565 0.94400
1.01000 0.18097 0.09632 0.02497 0.09549 0.17854 0.24678 0.26409 0.31978 0.39100 0.49675 0.59202 0.84425 1.18255 1.69451
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.06414 0.03608 0.02620 0.03984 0.06069 0.07939 0.09521 0.11116 0.12478 0.14830 0.19499 0.28590 0.44142 0.73195
0.60000 0.07171 0.03841 0.02649 0.04378 0.06932 0.08637 0.10408 0.12143 0.13698 0.16221 0.21480 0.32092 0.50474 0.85465
0.88000 0.08775 0.04477 0.02698 0.05297 0.08783 0.10207 0.12310 0.14278 0.16170 0.19495 0.26038 0.39754 0.63568 1.11300
0.92000 0.09196 0.04704 0.02708 0.05686 0.09333 0.10822 0.12895 0.15699 0.16945 0.20565 0.27546 0.41796 0.66209 1.15161
0.96000 0.09777 0.05073 0.02717 0.06318 0.10117 0.11637 0.13741 0.16011 0.18221 0.22122 0.29677 0.44670 0.68683 1.14493
0.98000 0.10250 0.05395 0.02720 0.06953 0.10743 0.12148 0.14447 0.17216 0.19246 0.23283 0.31721 0.47566 0.70013 1.07541
1.01000 0.18444 0.10075 0.03215 0.10254 0.18413 0.23341 0.26851 0.31634 0.36604 0.47633 0.59193 0.83502 1.15728 1.62998
</tableData>
</table>
</function>
<!-- elevator -->
<function name="aero/CDtot_elevator_-24">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.04625 0.03723 0.02587 0.01066 -0.03457 -0.02144 -0.02353 -0.03019 -0.03704 -0.04878 -0.05692 -0.06773 -0.07768 -0.11508
0.60000 0.04837 0.03947 0.02728 0.01058 -0.04362 -0.02408 -0.02581 -0.03273 -0.03972 -0.05241 -0.06190 -0.07489 -0.08457 -0.12566
0.88000 0.05401 0.04542 0.03114 0.01129 -0.06568 -0.02639 -0.02786 -0.03397 -0.04322 -0.05917 -0.07464 -0.09409 -0.09749 -0.12382
0.92000 0.05538 0.04733 0.03246 0.01179 -0.07198 -0.02555 -0.02733 -0.03353 -0.04328 -0.06097 -0.07879 -0.10194 -0.10116 -0.11440
0.96000 0.05695 0.04998 0.03445 0.01289 -0.08262 -0.02237 -0.02529 -0.03160 -0.04197 -0.06386 -0.08486 -0.11568 -0.10590 -0.09467
0.98000 0.05678 0.05159 0.03603 0.01428 -0.09339 -0.01835 -0.02186 -0.02838 -0.03973 -0.06648 -0.09064 -0.12879 -0.10992 -0.07207
1.01000 0.10860 0.09634 0.07981 0.06056 0.03611 0.02228 0.00681 -0.01066 -0.03078 -0.07995 -0.12160 -0.20101 -0.23793 -0.17616
</tableData>
</table>
</function>
<function name="aero/CDtot_elevator_-9.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.01982 0.01498 0.00677 -0.00490 -0.01106 -0.01514 -0.01848 -0.02144 -0.02391 -0.02691 -0.02509 -0.02331 -0.03135 -0.05754
0.60000 0.02133 0.01698 0.00803 -0.00562 -0.01268 -0.01718 -0.02071 -0.02416 -0.02680 -0.02967 -0.02755 -0.02436 -0.03376 -0.06121
0.88000 0.02488 0.02066 0.01129 -0.00720 -0.01638 -0.02086 -0.02502 -0.02840 -0.03374 -0.03696 -0.03433 -0.02516 -0.03499 -0.06244
0.92000 0.02579 0.02164 0.01216 -0.00769 -0.01686 -0.02148 -0.02592 -0.02951 -0.03545 -0.04005 -0.03761 -0.02484 -0.03363 -0.05820
0.96000 0.02707 0.02303 0.01326 -0.00866 -0.01700 -0.02177 -0.02681 -0.03083 -0.03778 -0.04620 -0.04433 -0.02278 -0.02911 -0.04858
0.98000 0.02772 0.02404 0.01406 -0.00998 -0.01649 -0.02217 -0.02708 -0.03156 -0.03971 -0.05250 -0.05154 -0.01978 -0.02336 -0.03747
1.01000 0.09104 0.04396 0.03055 0.01335 -0.00965 -0.02245 -0.03648 -0.05128 -0.06644 -0.09836 -0.10903 -0.06722 -0.05950 -0.09073
</tableData>
</table>
</function>
<function name="aero/CDtot_elevator_-3">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00569 0.00321 0.00055 -0.00291 -0.00497 -0.00635 -0.00726 -0.00814 -0.00900 -0.00799 -0.00622 -0.00838 -0.01276 -0.02403
0.60000 0.00662 0.00380 0.00069 -0.00455 -0.00580 -0.00721 -0.00827 -0.00930 -0.01022 -0.00812 -0.00652 -0.00873 -0.01335 -0.02644
0.88000 0.00884 0.00505 0.00105 -0.00679 -0.00763 -0.00912 -0.01042 -0.01062 -0.01304 -0.00902 -0.00663 -0.00902 -0.01395 -0.02683
0.92000 0.00942 0.00551 0.00117 -0.00763 -0.00805 -0.00961 -0.01097 -0.01106 -0.01372 -0.01015 -0.00657 -0.00867 -0.01334 -0.02447
0.96000 0.01031 0.00608 0.00136 -0.00901 -0.00852 -0.01010 -0.01170 -0.01159 -0.01473 -0.01324 -0.00690 -0.00762 -0.01138 -0.02058
0.98000 0.01083 0.00647 0.00151 -0.01032 -0.00874 -0.01103 -0.01214 -0.01366 -0.01542 -0.01646 -0.00739 -0.00581 -0.00931 -0.01529
1.01000 0.02046 0.01213 0.00404 -0.00355 -0.01227 -0.01659 -0.02099 -0.02544 -0.03023 -0.03982 -0.02677 -0.01526 -0.02113 -0.03335
</tableData>
</table>
</function>
<function name="aero/CDtot_elevator_1.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.00259 -0.00135 0.00000 0.00129 0.00268 0.00327 0.00378 0.00424 0.00404 0.00275 0.00293 0.00414 0.00644 0.01377
0.60000 -0.00296 -0.00150 0.00000 0.00156 0.00317 0.00394 0.00433 0.00483 0.00390 0.00276 0.00311 0.00443 0.00725 0.01485
0.88000 -0.00388 -0.00191 0.00000 0.00230 0.00423 0.00528 0.00561 0.00589 0.00426 0.00291 0.00319 0.00439 0.00735 0.01491
0.92000 -0.00412 -0.00202 0.00011 0.00258 0.00450 0.00563 0.00592 0.00622 0.00456 0.00292 0.00306 0.00427 0.00700 0.01419
0.96000 -0.00438 -0.00216 0.00016 0.00330 0.00494 0.00624 0.00639 0.00697 0.00586 0.00270 0.00551 0.00371 0.00612 0.01179
0.98000 -0.00455 -0.00225 0.00019 0.00399 0.00507 0.00598 0.00651 0.00735 0.00731 0.00264 0.00414 0.00301 0.00477 0.00932
1.01000 -0.00747 -0.00324 0.00075 0.01097 0.00889 0.01087 0.01299 0.01521 0.01730 0.01169 0.00610 0.00786 0.01129 0.01847
</tableData>
</table>
</function>
<function name="aero/CDtot_elevator">
<interpolate1d>
<property>fcs/surfaces/elevator-pos-deg</property>
<value>-24</value> <property>aero/CDtot_elevator_-24</property>
<value>-9.5</value> <property>aero/CDtot_elevator_-9.5</property>
<value>-3</value> <property>aero/CDtot_elevator_-3</property>
<value>0</value> <value>0</value>
<value>1.5</value> <property>aero/CDtot_elevator_1.5</property>
</interpolate1d>
</function>
<!-- flaps -->
<function name="aero/CDtot_flaps_20">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.02411 -0.00372 0.01634 0.03267 0.05568 0.06518 0.07499 0.08430 0.09201 0.11163 0.13925 0.21203 0.31664 0.37072
0.60000 -0.02884 -0.00473 0.02073 0.04201 0.06821 0.07778 0.08716 0.09482 0.10238 0.12558 0.15749 0.24537 0.37951 0.51545
0.88000 -0.03694 -0.00734 0.03691 0.08049 0.09339 0.10170 0.11024 0.11954 0.12667 0.15724 0.19970 0.32230 0.51476 0.83198
0.92000 -0.03905 -0.00803 0.04468 0.07350 0.10029 0.10958 0.11732 0.12687 0.13462 0.16673 0.21164 0.34284 0.53867 0.89372
0.96000 -0.04181 -0.00863 0.04614 0.15195 0.11297 0.12080 0.12800 0.13901 0.14760 0.17855 0.22490 0.36099 0.54544 0.89951
0.98000 -0.04409 -0.00834 0.07323 0.66397 0.12308 0.12952 0.13725 0.14591 0.15766 0.18610 0.23007 0.36347 0.51972 0.82904
1.01000 0.09529 0.06235 0.16114 0.17686 0.22128 0.23757 0.25583 0.27584 0.29773 0.34822 0.43124 0.69308 0.97498 1.39993
</tableData>
</table>
</function>
<function name="aero/CDtot_flaps_30">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.02388 0.00399 0.03032 0.05166 0.07767 0.08319 0.08997 0.09660 0.10251 0.12133 0.14830 0.22083 0.32576 0.37930
0.60000 -0.02859 0.00504 0.03876 0.06928 0.08823 0.09478 0.10020 0.10674 0.11362 0.13562 0.16743 0.25541 0.39024 0.52479
0.88000 -0.03595 0.00984 0.06835 0.08783 0.11101 0.11827 0.12477 0.13364 0.14056 0.16987 0.21409 0.33775 0.53145 0.84554
0.92000 -0.03733 0.01273 0.08170 0.09364 0.11926 0.12640 0.13300 0.14245 0.15039 0.18245 0.22772 0.36066 0.55792 0.90762
0.96000 -0.03848 0.01915 0.08979 0.29758 0.13284 0.13920 0.14626 0.15795 0.16595 0.19737 0.24671 0.38296 0.56863 0.91832
0.98000 -0.03781 0.02789 0.11346 0.48308 0.14448 0.14905 0.15941 0.16687 0.17862 0.20701 0.25218 0.38853 0.54774 0.85153
1.01000 0.16424 0.16794 0.25734 0.24182 0.27697 0.28791 0.30139 0.31726 0.33531 0.37988 0.45895 0.72046 1.00293 1.42098
</tableData>
</table>
</function>
<function name="aero/CDtot_flaps">
<interpolate1d>
<property>fcs/surfaces/flaps-pos-deg</property>
<value>0</value> <value>0</value>
<value>20</value> <property>aero/CDtot_flaps_20</property>
<value>30</value> <property>aero/CDtot_flaps_30</property>
</interpolate1d>
</function>
<!-- left-flaperon -->
<function name="aero/CDtot_left-flaperon_-51">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00922 0.01221 0.00513 -0.00272 -0.01026 -0.01137 -0.00963 -0.00694 -0.00327 -0.00498 -0.01082 -0.00727 -0.00760 -0.00814
0.60000 0.00862 0.01401 0.00635 -0.00407 -0.01209 -0.01151 -0.00857 -0.00781 -0.00504 0.01054 -0.00992 -0.00919 -0.00996 -0.01088
0.88000 0.00906 0.01792 0.00864 -0.00305 -0.00708 -0.01116 -0.01015 -0.01322 0.08116 0.00632 -0.01260 -0.01593 -0.01982 -0.02414
0.92000 0.00962 0.01943 0.01231 0.05720 -0.01086 -0.01169 -0.01055 -0.01634 0.12698 0.00515 -0.01444 -0.01912 -0.02386 -0.02848
0.96000 0.01291 0.02688 -0.01022 0.07314 -0.01532 -0.01368 -0.01211 0.10462 0.32305 0.00477 -0.01575 -0.02542 -0.03210 -0.04253
0.98000 0.02263 0.00551 0.02011 -0.00123 -0.01604 -0.01514 -0.00375 -0.01030 0.07839 0.00390 -0.01925 -0.03451 -0.04463 -0.06272
1.01000 0.02954 0.04481 0.07256 0.01585 0.02888 0.06296 0.04279 0.00937 -0.04336 -0.02463 0.00042 -0.08163 0.05270 0.04100
</tableData>
</table>
</function>
<function name="aero/CDtot_left-flaperon">
<interpolate1d>
<property>fcs/surfaces/left-flaperon-pos-deg</property>
<value>-51</value> <property>aero/CDtot_left-flaperon_-51</property>
<value>0</value> <value>0</value>
</interpolate1d>
</function>
<!-- right-flaperon -->
<function name="aero/CDtot_right-flaperon_-51">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00922 0.01218 0.00508 -0.00311 -0.01023 -0.01142 -0.00962 -0.00695 -0.00322 -0.00516 -0.01079 -0.00732 -0.00770 -0.00841
0.60000 0.00862 0.01401 0.00625 -0.00518 -0.01204 -0.01154 -0.00857 -0.00782 -0.00548 0.00944 -0.01002 -0.00922 -0.01008 -0.01096
0.88000 0.00903 0.01793 0.00856 -0.00365 0.00928 -0.01113 -0.01016 -0.01307 0.08087 0.00649 -0.01264 -0.01595 -0.01992 -0.02442
0.92000 0.00961 0.01941 0.01255 -0.00569 -0.01045 -0.01169 -0.01049 -0.01633 0.13139 0.00518 -0.01430 -0.01911 -0.02399 -0.02802
0.96000 0.01293 0.02678 -0.00928 0.00042 -0.01529 -0.01367 -0.01211 0.10017 0.31913 0.00490 -0.01588 -0.02542 -0.03212 -0.04270
0.98000 0.02085 0.00726 0.02029 -0.00057 -0.01604 -0.01456 -0.00358 -0.01042 0.08032 0.00415 -0.01935 -0.03428 -0.04457 -0.06287
1.01000 0.02954 0.04480 0.07258 0.01286 0.02901 0.06294 0.04259 0.00935 -0.04370 -0.02459 0.00129 -0.08145 0.05244 0.04085
</tableData>
</table>
</function>
<function name="aero/CDtot_right-flaperon">
<interpolate1d>
<property>fcs/surfaces/right-flaperon-pos-deg</property>
<value>-51</value> <property>aero/CDtot_right-flaperon_-51</property>
<value>0</value> <value>0</value>
</interpolate1d>
</function>
<!-- rudder -->
<function name="aero/CDtot_rudder_-35">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.00230 -0.00269 -0.00117 0.00051 0.00342 0.00218 0.00081 -0.00095 -0.00349 0.00778 0.01490 -0.00695 -0.00809 -0.00790
0.60000 -0.00117 -0.00111 0.00074 0.00471 0.00686 0.00574 0.00226 0.00023 -0.00333 0.02262 0.01986 -0.00607 -0.00883 -0.00946
0.88000 0.00857 0.01485 0.01958 0.03339 0.04114 0.02329 0.01489 0.01302 -0.05803 0.04207 0.00557 -0.00807 -0.01006 -0.01052
0.92000 0.01895 0.03300 0.03801 0.03902 0.03849 0.01447 0.00587 0.01025 0.08203 0.03085 0.00591 -0.00932 -0.01100 -0.01163
0.96000 0.03075 0.03792 0.02189 -0.02603 0.01639 0.01569 0.01311 0.01063 -0.00758 0.03673 -0.09264 -0.01475 -0.01446 -0.01510
0.98000 -0.06602 -0.06968 0.04297 -0.01296 0.06243 0.01741 0.12105 -0.48552 -0.06830 0.05538 0.03601 -0.02203 -0.01883 -0.01763
1.01000 -0.02094 -0.00737 0.00414 0.01842 0.02324 0.01217 0.02192 0.01076 0.01222 -0.03052 -0.05183 -0.05827 -0.10713 -0.09933
</tableData>
<tableData breakPoint="-5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00233 0.00285 0.00187 0.00355 0.00177 0.00380 0.00537 0.00188 0.00067 -0.00185 -0.00085 -0.00662 0.00048 0.00022
0.60000 0.00305 0.00368 0.00239 0.00660 0.00295 0.00651 0.00752 0.00181 0.00088 -0.00274 -0.00298 0.00000 0.00085 0.00028
0.88000 0.00622 0.00676 0.00990 0.04760 0.00459 0.00941 0.01297 -0.00092 -0.02119 -0.00537 -0.00107 0.00201 0.00310 0.00082
0.92000 0.00848 0.00831 0.02974 0.00493 0.00441 0.01704 0.01072 0.08853 -0.02981 -0.01380 0.00000 0.00224 0.00324 0.00057
0.96000 0.02194 -0.00589 0.03852 -0.07610 0.00984 0.00115 0.01199 0.12319 0.16315 0.09296 0.00265 0.00164 0.00270 0.00068
0.98000 -0.00246 0.03088 0.04643 -0.34121 0.02674 0.20197 0.16531 0.22040 0.18402 0.06558 0.00335 -0.00149 0.00243 -0.00079
1.01000 0.00546 0.00841 0.01002 0.03193 0.04712 0.02356 0.01153 0.02773 -0.03877 -0.02772 -0.04714 -0.04817 -0.02567 0.00041
</tableData>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00683 0.00747 0.00579 0.00264 0.00608 0.00587 0.00511 0.00280 0.01763 0.02273 0.00532 0.00403 0.00406 0.00285
0.60000 0.00799 0.00869 0.00710 0.00331 0.00733 0.00731 0.00652 0.00346 0.01372 0.02815 0.00487 0.00439 0.00559 0.00333
0.88000 0.01118 0.01230 0.01075 0.01135 0.01068 0.01085 0.01098 0.00713 0.12073 0.00520 0.00966 0.00855 0.00654 0.00480
0.92000 0.01239 0.01371 0.01128 0.01341 0.01145 0.01223 0.01263 0.00920 0.06787 0.00791 0.01101 0.00962 0.00729 0.00473
0.96000 0.01455 0.01643 0.00493 0.01784 0.01638 0.01484 0.01507 0.00790 -0.00782 0.01137 0.01298 0.01132 0.00874 0.00519
0.98000 0.01888 0.01608 0.01544 0.03102 0.01673 0.01631 0.01667 0.01662 0.00394 0.01381 0.01509 0.01276 0.00982 0.00552
1.01000 0.02973 0.03164 0.03282 0.03245 0.03338 0.03312 0.03276 0.03223 0.03126 0.02918 0.02631 0.02019 0.01380 0.00752
</tableData>
<tableData breakPoint="5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.01186 0.01221 0.05900 0.03658 0.00934 0.00854 0.00814 0.01173 0.01497 0.01522 0.01451 0.00488 0.00500 0.00302
0.60000 0.01359 0.01253 0.01160 0.03302 0.00927 0.01072 0.01036 0.01161 0.01361 0.02190 0.01661 0.00690 0.00570 0.00306
0.88000 0.01825 0.00979 0.03061 -0.03974 0.00830 0.01080 0.01081 0.02074 0.03417 -0.00290 0.00495 0.01035 0.00845 0.00486
0.92000 0.02094 0.00372 0.04608 0.05388 0.00619 0.02904 0.03246 0.03385 -0.28964 -0.00273 0.00465 0.01113 0.00887 0.00479
0.96000 0.03752 -0.00470 0.03276 0.11401 0.04540 0.01618 0.00709 0.22995 0.04027 -0.00251 0.00084 0.01152 0.00971 0.00558
0.98000 -0.00522 0.02519 0.02696 0.02709 0.01375 0.00082 0.03879 0.01779 0.06667 0.00351 -0.00810 0.01012 0.00937 0.00401
1.01000 0.02993 0.03561 0.04208 0.04623 0.03809 0.04294 0.00261 0.02919 -0.03790 -0.01795 -0.02613 -0.06225 -0.00989 0.01065
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.02534 0.05111 0.02771 0.02583 0.01722 0.01114 0.01517 0.02366 0.03143 0.03771 0.00019 0.02484 0.01107 0.01042
0.60000 0.02873 0.05982 0.03354 0.03360 0.02359 0.01595 0.01729 0.02992 0.03785 0.05446 -0.01231 0.06785 0.01173 0.00993
0.88000 0.04343 0.10709 0.07158 0.06071 0.06233 0.03269 0.02962 0.00884 0.00627 0.14185 -0.00855 0.01495 0.01399 0.00814
0.92000 0.05479 0.16090 0.05614 0.08028 0.05640 0.02792 0.02727 0.00659 0.00534 0.14200 -0.01418 0.01385 0.01326 0.00656
0.96000 0.04462 0.04205 0.05450 0.03805 0.05673 0.02636 0.03151 -0.00396 -0.02318 0.08447 -0.02589 0.00930 0.00979 0.00129
0.98000 -0.66116 0.03468 0.04042 0.02772 0.16103 0.01349 0.04739 0.14538 0.31568 0.01353 -0.03710 0.00197 0.00382 -0.00362
1.01000 0.01384 0.02608 0.03411 0.04029 0.03956 0.03664 0.03492 0.01574 0.02910 0.02359 -0.02808 -0.05810 -0.08979 -0.07223
</tableData>
</table>
</function>
<function name="aero/CDtot_rudder_35">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="-10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.02530 0.05078 0.02706 0.02639 0.01724 0.01130 0.01531 0.02402 0.03137 0.03754 0.00000 0.02475 0.01097 0.01127
0.60000 0.02860 0.05945 0.03334 0.03249 0.02395 0.01622 0.01755 0.02987 0.03790 0.05365 -0.01232 0.06654 0.01180 0.00988
0.88000 0.04336 0.10685 0.07156 0.06058 0.06228 0.03283 0.02840 0.00962 0.00640 0.13250 -0.00860 0.01487 0.01427 0.00817
0.92000 0.05457 0.16034 0.05677 0.08024 0.05662 0.02617 0.02734 0.00646 0.00524 0.14252 -0.01453 0.01409 0.01312 0.00646
0.96000 0.04455 0.04240 0.05479 0.03816 0.05688 0.02647 0.02916 -0.00428 -0.06126 0.08643 -0.02627 0.00923 0.00966 0.00159
0.98000 -0.35989 0.03406 0.04033 0.02931 0.16702 0.01365 0.04670 0.14337 0.32071 0.01298 -0.03726 0.00190 0.00380 -0.00279
1.01000 0.01390 0.02612 0.03418 0.04023 0.03951 0.03687 0.03544 0.01528 0.02922 0.02345 -0.02825 -0.05809 -0.08978 -0.07200
</tableData>
<tableData breakPoint="-5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.01183 0.01210 0.04924 0.03344 0.00927 0.00860 0.00821 0.01171 0.01505 0.01508 0.01488 0.00490 0.00513 0.00307
0.60000 0.01354 0.01247 0.01241 0.03328 0.00929 0.01075 0.01086 0.01162 0.01314 0.02194 0.01385 0.00692 0.00575 0.00287
0.88000 0.01821 0.00981 0.02003 48.98134 0.00854 0.01074 0.01086 0.02207 0.03321 -0.00281 0.00488 0.01043 0.00815 0.00465
0.92000 0.02096 0.00370 0.04679 0.05571 0.00617 0.02887 0.03218 0.03413 -0.27265 -0.00281 0.00453 0.01114 0.00871 0.00480
0.96000 0.03801 -0.00490 0.03278 0.11201 0.04474 0.01608 0.00688 0.19922 0.04456 -0.00257 0.00071 0.01174 0.00965 0.00555
0.98000 -0.00778 0.02678 0.02658 0.02659 0.01382 0.00095 0.03903 0.01794 0.06700 0.00356 -0.00823 0.01000 0.00926 0.00554
1.01000 0.02993 0.03557 0.04213 0.04630 0.03803 0.04077 0.00263 0.02938 -0.03751 -0.01752 -0.02600 -0.06223 -0.00977 0.01072
</tableData>
<tableData breakPoint="0.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00685 0.00748 0.00578 0.00660 0.00605 0.00601 0.00509 0.00275 0.01742 0.02305 0.00539 0.00405 0.00415 0.00282
0.60000 0.00801 0.00869 0.00709 0.00965 0.00738 0.00746 0.00658 0.00379 0.02573 0.02859 0.00484 0.00430 0.00557 0.00332
0.88000 0.01118 0.01230 0.01073 -0.00950 0.01082 0.01082 0.01089 0.00704 0.11256 0.00506 0.00963 0.00856 0.00661 0.00480
0.92000 0.01233 0.01369 0.01122 0.00961 0.01166 0.01225 0.01263 0.00941 0.06696 0.00778 0.01096 0.00965 0.00736 0.00471
0.96000 0.01449 0.01636 0.00492 0.02048 0.01603 0.01487 0.01505 0.00785 -0.00885 0.01102 0.01295 0.01095 0.00883 0.00516
0.98000 0.02953 0.01627 0.01544 0.03039 0.01688 0.01467 0.01623 0.01665 0.00308 0.01336 0.01513 0.01245 0.01001 0.00528
1.01000 0.02973 0.03163 0.03282 0.03395 0.03338 0.03311 0.03277 0.03226 0.03125 0.02844 0.02629 0.02019 0.01382 0.00754
</tableData>
<tableData breakPoint="5.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 0.00231 0.00284 0.00186 0.00357 0.00175 0.00379 0.00535 0.00188 0.00061 -0.00153 -0.00065 -0.00667 0.00051 0.00024
0.60000 0.00307 0.00367 0.00238 0.00686 0.00280 0.00646 0.00702 0.00190 0.00125 -0.00165 -0.00261 0.00000 0.00081 0.00030
0.88000 0.00623 0.00676 0.00995 0.04678 0.00443 0.00947 0.01302 -0.00044 -0.02101 -0.00568 -0.00093 0.00199 0.00352 0.00092
0.92000 0.00851 0.00828 0.02966 0.00842 0.00437 0.01684 0.00859 0.08942 -0.02966 -0.01323 0.00000 0.00225 0.00326 0.00067
0.96000 0.02175 -0.00595 0.03874 -0.07148 0.01021 0.00107 0.01131 0.13300 0.16050 0.08770 0.00268 0.00155 0.00275 0.00087
0.98000 -0.00361 0.03080 0.04625 -0.19632 0.02744 0.20696 0.16566 0.22316 0.18364 0.06517 0.00344 -0.00129 0.00254 -0.00106
1.01000 0.00553 0.00845 0.00999 0.03197 0.04716 0.02820 0.01157 0.02738 -0.03921 -0.02815 -0.04710 -0.04810 -0.02579 0.00040
</tableData>
<tableData breakPoint="10.00000">
-10.00 -5.00 0.00 5.00 10.00 12.50 15.00 17.50 20.00 25.00 30.00 40.00 50.00 60.00
0.20000 -0.00228 -0.00269 -0.00107 0.00048 0.00340 0.00209 0.00077 -0.00099 -0.00371 0.00774 0.01498 -0.00691 -0.00815 -0.00847
0.60000 -0.00114 -0.00108 0.00091 0.00454 0.00695 0.00571 0.00221 0.00024 -0.00336 0.02238 0.02011 -0.00602 -0.00878 -0.00945
0.88000 0.00858 0.01496 0.01990 0.03341 0.04121 0.02339 0.01494 0.01281 -0.06035 0.04048 0.00568 -0.00794 -0.01013 -0.01052
0.92000 0.01898 0.03299 0.03785 0.03914 0.03848 0.01471 0.00589 0.01385 0.08609 0.03036 0.00627 -0.00956 -0.01117 -0.01166
0.96000 0.03155 0.03800 0.02185 -0.02714 0.01611 0.01539 0.01310 0.01003 -0.00775 0.03832 -0.04159 -0.01473 -0.01433 -0.01521
0.98000 -0.06638 -0.09127 0.04275 -0.01291 0.06332 0.01746 0.12157 -0.65211 -0.06926 0.05407 0.03762 -0.02198 -0.01878 -0.01846
1.01000 -0.02092 -0.00721 0.00409 0.01850 0.02329 0.01249 0.02187 0.01103 0.01214 -0.03053 -0.05173 -0.05825 -0.10717 -0.09949
</tableData>
</table>
</function>
<function name="aero/CDtot_rudder">
<interpolate1d>
<property>fcs/surfaces/rudder-pos-deg</property>
<value>-35</value> <property>aero/CDtot_rudder_-35</property>
<value>0</value> <value>0</value>
<value>35</value> <property>aero/CDtot_rudder_35</property>
</interpolate1d>
</function>
<!-- slats -->
<function name="aero/CDtot_slats_27.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
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</table>
</function>
<function name="aero/CDtot_slats">
<interpolate1d>
<property>fcs/surfaces/slats-pos-deg</property>
<value>0</value> <value>0</value>
<value>27.5</value> <property>aero/CDtot_slats_27.5</property>
</interpolate1d>
</function>
<!-- CS -->
<!-- base -->
<function name="aero/CS_base">
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<independentVar lookup="table">aero/beta-deg</independentVar>
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0.88000 -0.00859 -0.02062 -0.02671 -0.02187 -0.01884 -0.03400 0.00233 -0.00527 0.04843 0.00092 0.02159 0.05008 0.09031 0.14223
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</tableData>
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</tableData>
</table>
</function>
<!-- elevator -->
<function name="aero/CS_elevator_-24">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
<tableData breakPoint="0.00000">
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0.20000 0.00000 0.00068 0.00000 0.00000 0.00000 0.00011 -0.00045 0.00016 0.00000 0.00000 0.00101 0.00000 0.00058 -0.00023
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0.88000 0.00000 -0.00000 0.00000 0.00000 0.00000 -0.00012 0.00000 0.00000 -0.00029 0.00027 -0.00000 0.00000 0.00013 -0.00033
0.92000 0.00000 -0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00011 0.00000 0.00000 0.00000 0.00000
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1.01000 0.00000 0.00000 0.00000 0.00000 -0.00000 -0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000 0.00000
</tableData>
</table>
</function>
<function name="aero/CS_elevator_-9.5">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
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</tableData>
</table>
</function>
<function name="aero/CS_elevator_-3">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">aero/alpha-deg</independentVar>
<independentVar lookup="table">aero/beta-deg</independentVar>
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