Richard Harrison 2016-11-16 1.0 Copyright (C) 2016 Richard Harrison, All rights reserved Built using VSPAERO. Aircraft origin for measurements is the nose VSPAERO notes: The aileron deflection is for left side down. Rudder deflection is LE right. Elevator is TE down. Controls Position Limits (deg.) Wing flaps Up 0 Down 39.5 Aileron Up 28 Down 12 Elevator Up 30 Down 20 Elevator trim tab Up 13 Down 32 Rudder Left 25 Right 25Max. RPM 2700 ClMax 1.632 Built with AeroTool 1.0.0.0: Options: AeroDetail=Medium, Flaps, WakeIterations=1 119.484367 3 31 3.854334 6.5 0 0.5 6.5 0 0.5 6.7175 0 0 6.2175 0 0 3511 14135 16505 293 985 6.9 -0.95 0 185 6.9 0.95 0 185 3.715 0 -4.5 1.0 0.5 0.02 2086 419 12.5 NONE 8.327 -4.048 -4.5 1.0 0.5 0.02 1586 449 0 LEFT 8.327 4.048 -4.5 1.0 0.5 0.02 1586 449 0 RIGHT 6.76 -15.8 0.49 1.2 1.212 1.413 886.5 197 6.76 15.8 0.49 1.2 1.212 1.413 886.5 197 9.23 -15.56 0.52 1.2 1.212 1.413 886.5 197 9.23 15.56 0.52 1.2 1.212 1.413 886.5 197 20.69 -5.38 0.71 1.2 1.212 1.413 886.5 197 20.69 5.38 0.71 1.2 1.212 1.413 886.5 197 18.39 0 -1.36 1.2 1.212 1.413 886.5 197 22.93 0 -0.39 1.2 1.212 1.413 886.5 197 22.93 0 4.4 1.2 1.212 1.413 886.5 197 20.73 0 4.38 1.2 1.212 1.413 886.5 197 8.03 0 2.44 1.2 1.212 1.413 886.5 197 0.22 0 0 1.2 1.212 1.413 886.5 197 0 0 0 0 0 0 0 1 2 0 0 0 0 0 0 6.2175 0 0 5 1 5 7.857 -5.64 -0.7144 87 1 23.8 7.857 5.64 -0.7144 87 1 23.8 position/aircraft-on-ground ne 0

systems/NWS/engaged

fcs/steer-cmd-norm gear/unit[0]/wheel-speed-fpssystems/NWS/engaged 0 1 0 0 12.5 40 0 12.5

fcs/steer-pos-deg

BASIC DRAG aero/alpha-degfcs/elevator-pos-deg -30 -20 -10 0 10 20 -10 0.10461900 0.09488900 0.07552900 0.05129900 0.04002900 0.04287900 -5 0.07610900 0.06680900 0.04776900 0.03542900 0.03438900 0.04471900 -2 0.06577900 0.05555900 0.04086900 0.03448900 0.03817900 0.05158900 0 0.06197900 0.05170900 0.04029900 0.03739900 0.04370900 0.05867900 2 0.06083900 0.05092900 0.04300900 0.04315900 0.05170900 0.06789900 5 0.06410900 0.05598900 0.05306900 0.05837900 0.06883900 0.08644900 7 0.07672269 0.07068950 0.07152089 0.07980108 0.09518180 0.11644965 10 0.13213805 0.12944165 0.13637525 0.15232895 0.17661260 0.20730020 12 0.19153877 0.19425443 0.20717789 0.24600605 0.26106737 0.29847029 15 0.32005064 0.33206407 0.35479087 0.38765324 0.42768997 0.47511772 17 0.42065012 0.44092287 0.47224605 0.51350097 0.56242298 0.61494660 20 0.53548899 0.57182619 0.62055399 0.67810929 0.74147469 0.80390919 25 0.91721336 0.97013824 1.03265299 1.10194886 1.17433436 1.22364799 30 1.35459914 1.42552409 1.50429749 1.58730809 1.65919604 1.69328624 45 2.40836798 2.50805774 2.60497406 2.64354542 2.66321630 2.67518318 50 2.81442014 2.92643630 2.99628590 3.02612606 3.04636190 3.05915054 DRAG INCREMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 7 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 12 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 15 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 17 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 20 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 25 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 30 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 45 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 -0.00177000 -0.00291000 -0.00316000 -0.00330000 -0.00322000 -0.00290000 -0.00178000 -5 0.00443000 0.00418000 0.00426000 0.00431000 0.00426000 0.00418000 0.00437000 -2 0.00962000 0.00955000 0.00987000 0.00998000 0.00987000 0.00955000 0.00951000 0 0.01209000 0.01355000 0.01397000 0.01413000 0.01397000 0.01354000 0.01289000 2 0.01719000 0.01799000 0.01830000 0.01851000 0.01830000 0.01799000 0.01717000 5 0.02733000 0.02505000 0.02515000 0.02410000 0.02515000 0.02505000 0.02793000 7 0.04095158 0.03257027 0.03245792 0.03234557 0.03268262 0.03257027 0.04094034 10 0.05609475 0.05320575 0.05330205 0.04601535 0.05330205 0.05322180 0.08119695 12 0.06353874 0.06983676 0.07519104 0.05889708 0.07519104 0.06983676 0.06604254 15 0.08919788 0.07764188 0.07831598 0.07576403 0.05691330 0.07766595 0.08876453 17 0.09175946 0.07773497 0.07656171 0.07626158 0.07647986 0.07773497 0.09208688 20 0.10024830 0.09148500 0.08403780 0.08384520 0.08406990 0.09129240 0.10021620 25 0.13417800 0.11780700 0.04261275 0.11483775 0.11672363 0.11820825 0.13397738 30 0.17098065 0.14377590 -0.01405980 0.15152805 -0.01401165 0.14387220 0.16963245 45 0.17950320 0.16548192 0.18484464 0.18474192 0.18412560 0.17883552 0.27349200 50 0.14072640 0.17498352 0.07216080 0.18484464 0.18279024 0.17518896 0.14067504 -10 -5 -2 0 2 5 10 -10 0.00551000 0.00294000 0.00231000 0.00208000 0.00225000 0.00295000 0.00550000 -5 0.02603000 0.02583000 0.02609000 0.02623000 0.02614000 0.02583000 0.02603000 -2 0.04244000 0.04228000 0.04301000 0.04325000 0.04301000 0.04228000 0.04233000 0 0.05251000 0.05375000 0.05453000 0.05486000 0.05453000 0.05375000 0.05251000 2 0.06314000 0.06412000 0.06462000 0.06504000 0.06462000 0.06412000 0.06312000 5 0.08293000 0.07558000 0.07498000 0.07360000 0.07498000 0.07558000 0.08293000 7 0.10891209 0.08393669 0.08180204 0.07907193 0.08180204 0.08393669 0.10888962 10 0.14079060 0.11901075 0.10520775 0.07551525 0.10520775 0.11901075 0.14048565 12 0.12403440 0.12823308 0.13959648 0.12380328 0.13959648 0.12823308 0.12376476 15 0.18612383 0.16245810 0.16428780 0.15882278 0.14288513 0.16250625 0.18569048 17 0.20662931 0.17702508 0.17066768 0.17094053 0.17200464 0.17536070 0.20695673 20 0.23959440 0.21927510 0.20319300 0.20380290 0.20322510 0.21901830 0.23953020 25 0.31425900 0.28127625 0.27890888 0.27044250 0.27858788 0.28199850 0.31389788 30 0.38996685 0.33849450 -0.00139635 0.35250615 -0.01223010 0.33830190 0.38553705 45 0.37117872 0.37164096 0.38324832 0.38304288 0.38206704 0.37158960 0.46521888 50 0.27934704 0.34447152 0.24755520 0.36198528 0.35823600 0.34457424 0.27929568 -10 -5 -2 0 2 5 10 -10 0.02188000 0.01797000 0.01702000 0.01675000 0.01689000 0.01775000 0.02187000 -5 0.05636000 0.05532000 0.05553000 0.05569000 0.05861000 0.05528000 0.05635000 -2 0.07850000 0.07606000 0.07660000 0.07682000 0.07660000 0.07606000 0.07841000 0 0.08744000 0.08586000 0.08623000 0.08620000 0.08623000 0.08585000 0.08745000 2 0.09627000 0.09397000 0.09387000 0.09428000 0.09387000 0.09396000 0.09625000 5 0.11272000 0.10108000 0.09943000 0.09767000 0.09943000 0.10107000 0.11272000 7 0.14699874 0.11659683 0.11079957 0.11019288 0.11081081 0.11652942 0.14696504 10 0.20344980 0.16727310 0.16162350 0.12175530 0.16163955 0.16727310 0.20348190 12 0.17337852 0.18073584 0.17478450 0.15964614 0.17478450 0.18073584 0.17310888 15 0.25644690 0.22052700 0.22247708 0.21455640 0.17230478 0.23624798 0.25601355 17 0.29091267 0.24581057 0.24114483 0.21792530 0.24106298 0.24581057 0.29121281 20 0.34558860 0.31438740 0.29166060 0.29332980 0.29159640 0.31409850 0.34552440 25 0.44394300 0.40040738 0.39651525 0.38977425 0.39571275 0.40129013 0.44354175 30 0.53364645 0.47264040 0.01439685 0.48978180 0.01507095 0.47307375 0.53186490 45 0.44898912 0.45099216 0.46516752 0.46470528 0.46444848 0.45217344 0.54302928 50 0.31401504 0.38407008 0.28710240 0.40163520 0.39778320 0.38407008 0.31396368 BASIC LIFT aero/alpha-degfcs/elevator-pos-deg -30 -20 -10 0 10 20 -10 -0.76264000 -0.75479000 -0.67030000 -0.50071000 -0.35159000 -0.22947000 -5 -0.41834000 -0.39870000 -0.25439000 -0.09576000 0.03936000 0.14753000 -2 -0.20709000 -0.16003000 -0.00406000 0.14680000 0.27467000 0.37535000 0 -0.06363000 0.00280000 0.16359000 0.31007000 0.43227000 0.52836000 2 0.08210000 0.17154000 0.32355000 0.47340000 0.59106000 0.68294000 5 0.30709000 0.43126000 0.58634000 0.73084000 0.83436000 0.92164000 7 0.46789000 0.60110000 0.75678000 0.89260000 1.00528000 1.09343000 10 0.69153000 0.82886000 0.98546000 1.12066000 1.23367000 1.32293000 12 0.88925000 1.04476000 1.19054000 1.32517000 1.41946000 1.49995000 15 1.19781000 1.34540000 1.47693000 1.58866000 1.66837000 1.74787000 17 1.32887000 1.47081000 1.59593000 1.70130000 1.78585000 1.84849000 20 1.34413000 1.48119000 1.60804000 1.71579000 1.80321000 1.86592000 25 1.47039000 1.59516000 1.70388000 1.79460000 1.86701000 1.89340000 30 1.53330000 1.64936000 1.74993000 1.83363000 1.88811000 1.89635000 45 1.70163000 1.80241000 1.88475000 1.90662000 1.91460000 1.91886000 50 1.75827000 1.85641000 1.90400000 1.91803000 1.92739000 1.93314000 LIFT INCREMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 7 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 12 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 15 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 17 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 20 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 25 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 30 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 45 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 0.20915000 0.22012000 0.22314000 0.22438000 0.22375000 0.22008000 0.20915000 -5 0.22066000 0.23232000 0.23729000 0.23761000 0.23726000 0.23232000 0.22091000 -2 0.22929000 0.23842000 0.24322000 0.24581000 0.24349000 0.23842000 0.23027000 0 0.24506000 0.24250000 0.24746000 0.24917000 0.24745000 0.24484000 0.23749000 2 0.24694000 0.24643000 0.25027000 0.25226000 0.25028000 0.24643000 0.24736000 5 0.26838000 0.24805000 0.25183000 0.24403000 0.25183000 0.24805000 0.27363000 7 0.25673000 0.24308000 0.24664000 0.24815000 0.24731000 0.24308000 0.25669000 10 0.20522000 0.21415000 0.23685000 0.20074000 0.23684000 0.21421000 0.22879000 12 0.20220000 0.21197000 0.22093000 0.21340000 0.22094000 0.21197000 0.20703000 15 0.12142000 0.07905000 0.07842000 0.07163000 0.06561000 0.07909000 0.12079000 17 0.03789000 0.00954000 0.00827000 0.00796000 0.00788000 0.00955000 0.03919000 20 -0.00802000 -0.01626000 -0.01893000 -0.01759000 -0.01889000 -0.01660000 -0.00803000 25 -0.01107000 -0.01402000 -0.03781000 -0.01598000 -0.01675000 -0.01403000 -0.01106000 30 -0.01047000 -0.01307000 0.05368000 -0.01327000 0.05361000 -0.01267000 -0.01085000 45 -0.00688000 -0.00466000 -0.00584000 -0.00701000 -0.00565000 -0.00917000 -0.00395000 50 -0.01799000 -0.00989000 0.16008000 -0.00654000 -0.00837000 -0.00963000 -0.01800000 -10 -5 -2 0 2 5 10 -10 0.57048000 0.59756000 0.60560000 0.60724000 0.60621000 0.59752000 0.57048000 -5 0.59990000 0.62451000 0.63456000 0.63701000 0.63433000 0.62452000 0.59989000 -2 0.62199000 0.63642000 0.64624000 0.65047000 0.64654000 0.63642000 0.62297000 0 0.63338000 0.63874000 0.64704000 0.65022000 0.64703000 0.63874000 0.63324000 2 0.63701000 0.62362000 0.62967000 0.63322000 0.62967000 0.62362000 0.63743000 5 0.61470000 0.55608000 0.55675000 0.54654000 0.55675000 0.55608000 0.61470000 7 0.51926000 0.44544000 0.43800000 0.42087000 0.43800000 0.44545000 0.51919000 10 0.32787000 0.30885000 0.28321000 0.15903000 0.28320000 0.30886000 0.32643000 12 0.20892000 0.20810000 0.22960000 0.22710000 0.22962000 0.20809000 0.20882000 15 0.12977000 0.06538000 0.06891000 0.05678000 0.05610000 0.06548000 0.12913000 17 0.03931000 -0.01526000 -0.02203000 -0.02322000 -0.02168000 -0.01618000 0.03982000 20 -0.02448000 -0.03954000 -0.04460000 -0.04092000 -0.04455000 -0.03987000 -0.02448000 25 -0.02392000 -0.03093000 -0.03712000 -0.03502000 -0.03711000 -0.03093000 -0.02392000 30 -0.02159000 -0.02771000 0.11376000 -0.02838000 0.11901000 -0.02733000 -0.02297000 45 -0.01346000 -0.01745000 -0.01155000 -0.01374000 -0.01117000 -0.01745000 -0.01053000 50 -0.03125000 -0.01757000 0.15305000 -0.01222000 -0.01540000 -0.01758000 -0.03126000 -10 -5 -2 0 2 5 10 -10 0.97650000 1.01605000 1.02715000 1.02958000 1.02789000 1.01634000 0.97649000 -5 0.97310000 0.99588000 1.00596000 1.00862000 1.03760000 0.99614000 0.97320000 -2 0.94346000 0.93359000 0.93959000 0.94333000 0.93989000 0.93359000 0.94410000 0 0.88282000 0.85480000 0.85814000 0.85958000 0.85813000 0.85477000 0.88268000 2 0.82000000 0.76507000 0.76575000 0.76931000 0.76575000 0.76501000 0.82042000 5 0.66985000 0.58607000 0.57800000 0.56426000 0.57800000 0.58607000 0.66985000 7 0.52941000 0.48520000 0.45715000 0.45864000 0.45715000 0.48298000 0.52931000 10 0.36359000 0.33098000 0.33293000 0.17750000 0.33291000 0.33100000 0.36359000 12 0.18796000 0.19530000 0.17528000 0.17901000 0.17530000 0.19529000 0.18790000 15 0.12180000 0.03304000 0.03667000 0.01951000 -0.00827000 0.01812000 0.12113000 17 0.02446000 -0.04557000 -0.05139000 -0.06869000 -0.05178000 -0.04556000 0.02572000 20 -0.03685000 -0.05842000 -0.06591000 -0.05993000 -0.06589000 -0.05873000 -0.03688000 25 -0.03303000 -0.04326000 -0.05205000 -0.04968000 -0.05208000 -0.04326000 -0.03303000 30 -0.03092000 -0.03746000 0.15162000 -0.03839000 0.15123000 -0.03747000 -0.03122000 45 -0.01594000 -0.01987000 -0.01413000 -0.01640000 -0.01394000 -0.02013000 -0.01301000 50 -0.02941000 -0.01814000 0.15195000 -0.01345000 -0.01650000 -0.01833000 -0.02942000 BASIC PITCHING MOMENT aero/alpha-degfcs/elevator-pos-deg -30 -20 -10 0 10 20 -10 0.63094333 0.60709333 0.53875667 0.35533000 0.18906667 0.07592333 -5 0.46139667 0.44653667 0.29489000 0.12948000 -0.00810000 -0.11380667 -2 0.40127667 0.35709667 0.19308667 0.03633000 -0.09293667 -0.19136000 0 0.34978000 0.28277333 0.10967000 -0.04573000 -0.16085667 -0.26940333 2 0.33294000 0.24299000 0.08096333 -0.07062000 -0.18935333 -0.27930667 5 0.23558000 0.11666333 -0.06056000 -0.20531000 -0.29666000 -0.40774333 7 0.24708000 0.11053000 -0.05071333 -0.18990000 -0.30367333 -0.39095333 10 0.19406000 0.07284667 -0.11520000 -0.25742000 -0.34103667 -0.46630000 12 0.15000000 -0.00903667 -0.15759333 -0.28835000 -0.38784333 -0.46706667 15 -0.08328667 -0.20032333 -0.37293333 -0.48774000 -0.53755000 -0.64892000 17 -0.00259000 -0.14923667 -0.27896667 -0.38840000 -0.47617333 -0.54105333 20 -0.02997000 -0.13879000 -0.31676333 -0.43488000 -0.48296333 -0.60133667 25 -0.16618333 -0.29417333 -0.40627667 -0.50041000 -0.57614667 -0.60373000 30 -0.39420333 -0.46940333 -0.61531000 -0.70174000 -0.70907667 -0.76602667 45 -0.55640667 -0.60242333 -0.72092333 -0.73930000 -0.69731000 -0.74517333 50 -0.44948667 -0.53075000 -0.57007000 -0.57964000 -0.58481667 -0.58720000 PITCHING MOMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 7 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 12 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 15 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 17 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 20 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 25 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 30 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 45 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 -0.04185000 -0.06110000 -0.02720000 -0.07045000 -0.02795000 -0.06108000 -0.04185000 -5 -0.00822000 -0.02570000 -0.03672000 -0.03966000 -0.03669000 -0.02571000 -0.00821000 -2 -0.01959000 -0.02577000 -0.03737000 -0.04297000 -0.03773000 -0.02576000 -0.01966000 0 -0.00490000 0.00158000 -0.03630000 -0.01532000 -0.03630000 -0.00321000 -0.00380000 2 -0.04294000 -0.02041000 -0.03097000 -0.03617000 -0.03097000 -0.02040000 -0.04317000 5 -0.02712000 0.05520000 -0.01383000 0.04855000 -0.01382000 0.05520000 -0.04496000 7 -0.03417000 0.02662000 0.01906000 0.01465000 0.01468000 0.02663000 -0.03405000 10 0.23829000 0.23043000 0.06734000 0.26902000 0.06735000 0.23017000 0.21018000 12 0.08891000 0.03955000 -0.00022000 -0.00010000 -0.00024000 0.03956000 0.06632000 15 0.08918000 0.13540000 -0.00387000 0.14133000 0.00869000 0.13525000 0.09105000 17 -0.02920000 0.00250000 0.00286000 0.00406000 0.00282000 0.00250000 -0.02912000 20 0.11940000 0.12848000 -0.00166000 0.13209000 -0.00168000 0.12856000 0.11944000 25 -0.02596000 -0.01363000 -0.00449000 -0.00958000 -0.00858000 -0.01385000 -0.02586000 30 0.11795000 0.12592000 -0.05050000 0.12705000 -0.05047000 0.12652000 0.11804000 45 0.11079000 0.10228000 -0.03410000 0.10636000 -0.03374000 0.10712000 0.06554000 50 -0.00846000 -0.02736000 -0.14042000 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0.11595000 -0.00085000 0.12498000 -0.00089000 0.11609000 0.08701000 25 -0.06349000 -0.03629000 -0.02434000 -0.02214000 -0.02436000 -0.03669000 -0.06330000 30 0.08042000 0.09881000 -0.11432000 0.10126000 -0.11758000 0.09953000 0.08092000 45 0.07446000 0.07233000 -0.07161000 0.06991000 -0.07098000 0.07235000 0.02922000 50 -0.01967000 -0.05557000 -0.17004000 -0.06227000 -0.05941000 -0.05561000 -0.01969000 -10 -5 -2 0 2 5 10 -10 -0.21873000 -0.26980000 -0.24711000 -0.29232000 -0.24847000 -0.27238000 -0.21872000 -5 -0.21058000 -0.22255000 -0.24081000 -0.24765000 -0.27321000 -0.22321000 -0.21075000 -2 -0.24748000 -0.17791000 -0.19317000 -0.20220000 -0.19358000 -0.17790000 -0.24644000 0 -0.19978000 -0.09286000 -0.13371000 -0.10188000 -0.13370000 -0.09244000 -0.19973000 2 -0.21871000 -0.03647000 -0.04948000 -0.05909000 -0.04948000 -0.03608000 -0.21893000 5 -0.01732000 0.21554000 0.16495000 0.24414000 0.16496000 0.21554000 -0.01734000 7 0.11380000 0.21753000 0.28435000 0.28091000 0.28434000 0.21631000 0.11411000 10 0.28280000 0.32232000 0.23299000 0.83140000 0.23290000 0.32227000 0.28281000 12 0.34471000 0.27017000 0.32378000 0.28245000 0.32373000 0.27021000 0.34399000 15 0.07616000 0.25348000 0.09502000 0.27540000 0.24559000 0.24060000 0.07813000 17 -0.08185000 0.05358000 0.06192000 0.14484000 0.06190000 0.05360000 -0.08175000 20 0.06418000 0.11350000 0.00824000 0.12646000 0.00843000 0.11366000 0.06426000 25 -0.08989000 -0.05179000 -0.03421000 -0.03695000 -0.03392000 -0.05228000 -0.08966000 30 0.05539000 0.07966000 -0.15598000 0.08340000 -0.15576000 0.07949000 0.05562000 45 0.05958000 0.05726000 -0.08712000 0.05480000 -0.08675000 0.05719000 0.01433000 50 -0.02440000 -0.06277000 -0.17694000 -0.06910000 -0.06631000 -0.06264000 -0.02442000 PITCH DAMPING DERIVATIVE aero/qb aero/alpha-deg -10 22.19439670 -5 18.31365680 -2 16.95503250 0 17.12110580 2 15.32236540 5 15.64242200 7 14.86027160 10 16.10256230 12 13.55877550 15 8.25190770 17 11.05276140 20 11.83534860 25 9.81168450 30 5.51306100 45 -3.67420020 50 -3.46417220 BASIC ROLLING MOMENT aero/alpha-degaero/beta-deg -10 -5 -2 0 2 5 10 -10 0.01185000 0.00620000 0.00239000 0.00000000 -0.00252000 -0.00619000 -0.01185000 -5 0.01163000 0.00612000 0.00251000 0.00000000 -0.00251000 -0.00612000 -0.01163000 -2 0.01122000 0.00607000 0.00241000 0.00000000 -0.00248000 -0.00607000 -0.01147000 0 0.01160000 0.00605000 0.00245000 -0.00001000 -0.00245000 -0.00605000 -0.01157000 2 0.01171000 0.00613000 0.00242000 0.00000000 -0.00242000 -0.00613000 -0.01180000 5 0.01350000 0.00623000 0.00246000 -0.00378000 -0.00246000 -0.00623000 -0.01350000 7 0.01716000 0.00650000 0.00292000 0.00000000 -0.00292000 -0.00650000 -0.01716000 10 0.02101000 0.00528000 0.00274000 0.00000000 -0.00274000 -0.00528000 -0.02101000 12 0.02223000 0.00805000 0.00374000 -0.00085000 -0.00374000 -0.00805000 -0.02284000 15 0.01735000 0.00695000 0.00225000 0.00000000 -0.00389000 -0.00695000 -0.01765000 17 0.00792000 0.00246000 0.00068000 0.00000000 -0.00074000 -0.00246000 -0.00814000 20 0.00343000 0.00413000 -0.00029000 0.00000000 0.00030000 -0.00410000 -0.00343000 25 0.00512000 0.00207000 -0.00017000 0.00000000 0.00021000 -0.00209000 -0.00511000 30 0.00697000 0.00329000 0.00290000 0.00001000 -0.00294000 -0.00329000 -0.00697000 45 0.01556000 0.00710000 0.00312000 0.00000000 -0.00307000 -0.00711000 -0.01772000 50 0.00182000 0.01037000 0.00139000 0.00000000 -0.00444000 -0.01039000 -0.00191000 ROLLING MOMENT DUE TO AILERON DEFLECTION fcs/aileron-pos-deg aero/alpha-deg -10 0.00513600 -5 0.00519600 -2 0.00522240 0 0.00524000 2 0.00524560 5 0.00555440 7 0.00524880 10 0.00500160 12 0.00459680 15 0.00300720 17 0.00185680 20 0.00062880 25 0.00000000 30 -0.00002720 45 -0.00030720 50 -0.00039120 ROLLING MOMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 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0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 -0.00112000 -0.00066000 -0.00015000 0.00000000 0.00028000 0.00065000 0.00111000 -5 -0.00117000 -0.00076000 -0.00034000 0.00000000 0.00034000 0.00076000 0.00128000 -2 -0.00105000 -0.00079000 -0.00028000 0.00000000 0.00036000 0.00079000 0.00130000 0 -0.00375000 -0.00082000 -0.00036000 0.00001000 0.00036000 -0.00063000 0.00124000 2 -0.00111000 -0.00087000 -0.00038000 0.00000000 0.00038000 0.00087000 0.00120000 5 -0.00105000 -0.00110000 -0.00026000 0.00378000 0.00026000 0.00110000 -0.00090000 7 0.00028000 -0.00164000 -0.00026000 0.00000000 -0.00030000 0.00164000 -0.00028000 10 -0.00089000 -0.00064000 -0.00026000 0.00001000 0.00026000 0.00062000 0.00492000 12 -0.00484000 -0.00408000 -0.00141000 0.00084000 0.00141000 0.00408000 0.00462000 15 -0.01092000 -0.00443000 -0.00195000 0.00000000 0.00359000 0.00444000 0.01125000 17 -0.00231000 -0.00040000 -0.00022000 0.00000000 0.00028000 0.00040000 0.00254000 20 0.00065000 0.00021000 0.00009000 0.00000000 -0.00010000 -0.00022000 -0.00065000 25 0.00069000 0.00038000 0.00733000 0.00000000 -0.00014000 -0.00038000 -0.00069000 30 0.00052000 0.00033000 0.00010000 -0.00001000 -0.00011000 -0.00043000 -0.00052000 45 0.00022000 0.00038000 -0.00004000 0.00000000 0.00005000 -0.00015000 0.00193000 50 0.00068000 0.00004000 0.00308000 0.00000000 0.00002000 -0.00004000 -0.00068000 -10 -5 -2 0 2 5 10 -10 -0.00367000 -0.00206000 -0.00074000 0.00000000 0.00087000 0.00205000 0.00367000 -5 -0.00404000 -0.00228000 -0.00097000 0.00000000 0.00116000 0.00228000 0.00404000 -2 -0.00378000 -0.00231000 -0.00093000 0.00000000 0.00100000 0.00231000 0.00403000 0 -0.00449000 -0.00317000 -0.00130000 0.00001000 0.00130000 0.00317000 0.00446000 2 -0.00525000 -0.00335000 -0.00135000 0.00000000 0.00135000 0.00335000 0.00534000 5 -0.00736000 -0.00592000 -0.00137000 0.00378000 0.00137000 0.00592000 0.00736000 7 -0.00586000 -0.00720000 0.00194000 0.00001000 -0.00194000 0.00720000 0.00586000 10 -0.00332000 0.00198000 -0.00076000 0.00001000 0.00076000 -0.00198000 0.00299000 12 -0.01260000 -0.01032000 -0.00188000 0.00084000 0.00188000 0.01032000 0.01321000 15 -0.01199000 -0.00465000 -0.00220000 -0.00001000 0.00384000 0.00467000 0.01231000 17 -0.00434000 -0.00092000 -0.00062000 0.00000000 0.00050000 0.00108000 0.00466000 20 0.00112000 0.00038000 0.00018000 0.00000000 -0.00020000 -0.00039000 -0.00112000 25 0.00129000 0.00072000 0.00024000 -0.00013000 -0.00024000 -0.00072000 -0.00130000 30 0.00085000 0.00060000 0.00016000 0.00000000 -0.00018000 -0.00070000 -0.00093000 45 0.00014000 0.00015000 -0.00013000 0.00000000 0.00015000 -0.00014000 0.00202000 50 0.00103000 -0.00007000 0.00299000 0.00000000 0.00010000 0.00008000 -0.00103000 -10 -5 -2 0 2 5 10 -10 -0.00799000 -0.00452000 -0.00174000 0.00000000 0.00169000 0.00387000 0.00799000 -5 -0.00873000 -0.00475000 -0.00198000 0.00000000 0.00427000 0.00458000 0.00874000 -2 -0.01074000 -0.00592000 -0.00241000 0.00000000 0.00248000 0.00592000 0.01110000 0 -0.01063000 -0.00597000 -0.00240000 -0.00201000 0.00240000 0.00601000 0.01060000 2 -0.01059000 -0.00653000 -0.00257000 0.00000000 0.00257000 0.00651000 0.01068000 5 -0.01172000 -0.00791000 -0.00127000 0.00378000 0.00127000 0.00791000 0.01172000 7 -0.00790000 -0.00637000 -0.00031000 0.00000000 0.00031000 0.00566000 0.00790000 10 -0.00721000 0.00115000 -0.00083000 0.00001000 0.00083000 -0.00114000 0.00720000 12 -0.01310000 -0.00970000 -0.00017000 0.00084000 0.00017000 0.00970000 0.01370000 15 -0.01261000 -0.00544000 -0.00274000 -0.00001000 -0.00151000 0.00888000 0.01292000 17 -0.00426000 -0.00101000 -0.00043000 -0.00269000 0.00048000 0.00101000 0.00448000 20 0.00139000 0.00046000 0.00026000 0.00000000 -0.00027000 -0.00047000 -0.00138000 25 0.00161000 0.00091000 0.00029000 0.00000000 -0.00030000 -0.00091000 -0.00161000 30 0.00098000 0.00070000 0.00017000 0.00000000 -0.00019000 -0.00071000 -0.00100000 45 -0.00021000 -0.00001000 -0.00023000 0.00000000 0.00023000 0.00003000 0.00236000 50 0.00069000 -0.00032000 0.00288000 0.00000000 0.00021000 0.00033000 -0.00069000 ROLLING MOMENT DUE TO RUDDER DEFLECTION fcs/rudder-pos-deg aero/alpha-degaero/beta-deg -10 -5 -2 0 2 5 10 -10 0.00026767 0.00027133 0.00026800 0.00023600 0.00027200 0.00026633 0.00025633 -5 0.00020833 0.00021100 0.00021200 0.00021167 0.00021067 0.00020667 0.00019933 -2 0.00016800 0.00017967 0.00017800 0.00018133 0.00017767 0.00017500 0.00017200 0 0.00015933 0.00016067 0.00016133 0.00015967 0.00015967 0.00015933 0.00015567 2 0.00013700 0.00013367 0.00014433 0.00014233 0.00014333 0.00014367 0.00014000 5 0.00011267 0.00012233 0.00012467 -0.00000167 0.00012533 0.00012367 0.00011000 7 0.00006067 0.00010933 0.00011300 0.00011733 0.00011367 0.00011200 0.00009000 10 0.00010533 0.00008700 0.00010133 0.00010333 0.00010367 0.00009333 0.00009900 12 0.00010500 0.00008800 0.00015067 0.00006633 0.00010633 0.00009467 0.00007733 15 0.00007667 0.00007867 0.00008800 0.00008667 0.00004000 0.00008733 0.00006933 17 0.00010033 0.00009033 0.00009267 0.00009533 0.00009767 0.00009867 0.00007800 20 0.00009667 0.00009333 0.00008833 0.00008533 0.00009633 0.00010067 0.00009433 25 0.00008967 0.00008500 0.00006400 0.00014267 0.00008633 0.00008933 0.00008000 30 0.00007600 0.00009233 0.00059267 0.00010100 0.00055033 0.00008667 0.00000900 45 0.00005033 0.00003800 0.00007600 0.00001700 0.00007967 0.00003000 -0.00003400 50 -0.00018900 0.00104233 -0.00007467 0.00003200 0.00002633 0.00001600 -0.00008067 ROLL DAMPING DERIVATIVE aero/pb aero/alpha-deg -10 -0.42332690 -5 -0.43050840 -2 -0.43701580 0 -0.44234510 2 -0.44867170 5 -0.45735850 7 -0.46271800 10 -0.44924330 12 -0.44193890 15 -0.28392020 17 -0.15664700 20 -0.00471490 25 0.04855610 30 0.05393250 45 0.09623550 50 0.10788440 ROLLING MOMENT DUE TO YAW RATE aero/rb aero/alpha-deg -10 0.00043810 -5 0.04769820 -2 0.07673290 0 0.09946900 2 0.11557790 5 0.14743950 7 0.16499840 10 0.19483380 12 0.21525940 15 0.17415060 17 0.08633990 20 0.02482180 25 0.04886440 30 -0.04077830 45 0.06426270 50 0.08553350 BASIC SIDE FORCE aero/alpha-degaero/beta-degfcs/elevator-pos-deg -10 -5 -2 0 2 5 10 -10 0.06426000 0.03319000 0.01360000 0.00000000 -0.01360000 -0.03320000 -0.06417000 -5 0.07052000 0.03764000 0.01579000 0.00000000 -0.01579000 -0.03758000 -0.07036000 -2 0.07073000 0.03936000 0.01643000 0.00000000 -0.01643000 -0.03937000 -0.07074000 0 0.07353000 0.04078000 0.01631000 0.00000000 -0.01631000 -0.04086000 -0.07354000 2 0.07346000 0.04119000 0.01571000 0.00001000 -0.01550000 -0.04120000 -0.07336000 5 0.06856000 0.03877000 0.01636000 -0.00002000 -0.01636000 -0.03877000 -0.06843000 7 0.03726000 0.03931000 0.01498000 -0.00010000 -0.01493000 -0.03930000 -0.03730000 10 0.07362000 0.03600000 0.01221000 -0.00006000 -0.01220000 -0.03599000 -0.07364000 12 0.07997000 0.03626000 -0.00998000 -0.00008000 0.00997000 -0.03623000 -0.07997000 15 0.06749000 0.03976000 0.01193000 -0.00006000 -0.01193000 -0.03976000 -0.06740000 17 0.05933000 0.02891000 0.01323000 0.00003000 -0.01319000 -0.02890000 -0.05931000 20 0.05239000 0.02345000 0.00633000 -0.00010000 -0.00625000 -0.02322000 -0.05238000 25 0.04237000 0.03333000 0.01654000 -0.00002000 -0.01498000 -0.03345000 -0.04235000 30 0.02621000 -0.00109000 0.03431000 0.00000000 -0.03215000 0.00099000 -0.02616000 45 0.00559000 -0.01850000 -0.01519000 0.00008000 0.01444000 0.01865000 -0.00552000 50 -0.21380000 -0.01060000 -0.01303000 -0.00002000 0.01300000 0.01082000 0.29356000 -10 -5 -2 0 2 5 10 -10 0.06594000 0.03405000 0.01394000 0.00000000 -0.01427000 -0.03406000 -0.06597000 -5 0.07255000 0.03869000 0.01625000 0.00000000 -0.01625000 -0.03870000 -0.07257000 -2 0.07296000 0.04075000 0.01703000 -0.00010000 -0.01706000 -0.04076000 -0.07298000 0 0.07604000 0.04231000 0.01709000 0.00000000 -0.01707000 -0.04232000 -0.07605000 2 0.07570000 0.04269000 0.01615000 0.00001000 -0.01616000 -0.04270000 -0.07570000 5 0.07014000 0.03997000 0.01665000 -0.00010000 -0.01685000 -0.03997000 -0.07014000 7 0.04047000 0.04019000 0.01533000 -0.00010000 -0.01536000 -0.04018000 -0.03956000 10 0.07565000 0.03675000 0.01291000 -0.00006000 -0.01289000 -0.03674000 -0.07566000 12 0.08139000 0.03666000 -0.00988000 -0.00008000 0.00986000 -0.03663000 -0.08138000 15 0.06763000 0.03905000 0.01254000 -0.00006000 -0.01254000 -0.03905000 -0.06760000 17 0.05937000 0.02878000 0.01316000 0.00003000 -0.01312000 -0.02876000 -0.05936000 20 0.05251000 0.02376000 0.00642000 -0.00011000 -0.00640000 -0.02354000 -0.05249000 25 0.04243000 0.03264000 0.00886000 -0.00002000 -0.01457000 -0.03277000 -0.04240000 30 0.02681000 -0.00088000 0.03227000 0.00000000 -0.03013000 0.00075000 -0.02677000 45 0.00828000 -0.01913000 -0.01391000 0.00008000 0.01318000 0.01929000 -0.00821000 50 -0.30565000 -0.01110000 -0.01317000 -0.00001000 0.01314000 0.01131000 0.30892000 -10 -5 -2 0 2 5 10 -10 0.07130000 0.03584000 0.01462000 0.00000000 -0.01417000 -0.03577000 -0.06958000 -5 0.07568000 0.04063000 0.01706000 0.00000000 -0.01706000 -0.04064000 -0.07612000 -2 0.07576000 0.04251000 0.01784000 0.00000000 -0.01784000 -0.04258000 -0.07580000 0 0.07861000 0.04403000 0.01773000 0.00000000 -0.01774000 -0.04403000 -0.07862000 2 0.07947000 0.04418000 0.01690000 0.00308000 -0.01691000 -0.04354000 -0.07767000 5 0.07086000 0.04101000 0.01705000 -0.00002000 -0.01729000 -0.04101000 -0.07086000 7 0.03964000 0.04100000 0.01535000 -0.00011000 -0.01535000 -0.04092000 -0.03967000 10 0.07693000 0.03749000 0.01337000 -0.00018000 -0.01336000 -0.03748000 -0.07695000 12 0.08229000 0.03669000 -0.00863000 -0.00007000 0.00862000 -0.03666000 -0.08224000 15 0.06710000 0.03802000 0.01304000 -0.00006000 -0.01303000 -0.03804000 -0.06711000 17 0.05882000 0.02835000 0.01295000 0.00003000 -0.01292000 -0.02834000 -0.05879000 20 0.05217000 0.02384000 0.00648000 -0.00014000 -0.00647000 -0.02358000 -0.05215000 25 0.04214000 0.03180000 0.01555000 -0.00002000 -0.01378000 -0.03194000 -0.04211000 30 0.02712000 -0.00046000 0.03029000 0.00001000 -0.02816000 0.00067000 -0.02708000 45 0.01077000 -0.01979000 -0.01280000 0.00007000 0.01221000 0.01991000 -0.01071000 50 -0.31418000 -0.01059000 -0.01315000 -0.00001000 0.01316000 0.01141000 0.32206000 -10 -5 -2 0 2 5 10 -10 0.07341000 0.03790000 0.01523000 0.00000000 -0.01548000 -0.03790000 -0.07343000 -5 0.07844000 0.04203000 0.01765000 0.00000000 -0.01765000 -0.04204000 -0.07846000 -2 0.07653000 0.04377000 0.01830000 0.00000000 -0.01842000 -0.04378000 -0.07721000 0 0.07996000 0.04513000 0.01826000 -0.00002000 -0.01827000 -0.04513000 -0.07988000 2 0.07820000 0.04509000 0.01738000 0.00001000 -0.01739000 -0.04510000 -0.07840000 5 0.07051000 0.04150000 0.01738000 -0.00528000 -0.01738000 -0.04150000 -0.07050000 7 0.03876000 0.04116000 0.01513000 -0.00011000 -0.01513000 -0.04116000 -0.03880000 10 0.07747000 0.03797000 0.01368000 -0.00008000 -0.01367000 -0.03796000 -0.07748000 12 0.08255000 0.03636000 -0.00752000 -0.00445000 0.00750000 -0.03632000 -0.08281000 15 0.06593000 0.03671000 0.01339000 -0.00007000 -0.01969000 -0.03673000 -0.06600000 17 0.05789000 0.02762000 0.01264000 0.00003000 -0.01253000 -0.02761000 -0.05770000 20 0.05140000 0.02371000 0.00647000 -0.00010000 -0.00647000 -0.02350000 -0.05137000 25 0.04154000 0.03083000 0.01497000 -0.00002000 -0.01354000 -0.03098000 -0.04150000 30 0.02676000 -0.00080000 0.02838000 0.00001000 -0.02627000 0.00069000 -0.02714000 45 0.01472000 -0.01958000 -0.01159000 0.00007000 0.01097000 0.01974000 -0.00764000 50 -0.33195000 -0.01072000 0.00096000 0.00004000 0.01291000 0.01093000 0.33517000 -10 -5 -2 0 2 5 10 -10 0.07558000 0.03897000 0.01584000 0.00000000 -0.01585000 -0.03888000 -0.07521000 -5 0.07907000 0.04251000 0.01786000 0.00000000 -0.01787000 -0.04252000 -0.07893000 -2 0.07707000 0.04416000 0.01979000 0.00000000 -0.01894000 -0.04417000 -0.07708000 0 0.07972000 0.04550000 0.01851000 0.00000000 -0.01851000 -0.04551000 -0.07972000 2 0.07786000 0.04538000 0.01802000 0.00001000 -0.01761000 -0.04538000 -0.07772000 5 0.06906000 0.04089000 0.01730000 -0.00002000 -0.01730000 -0.04134000 -0.06906000 7 0.03676000 0.04090000 0.01471000 -0.00011000 -0.01470000 -0.04090000 -0.03679000 10 0.07704000 0.03807000 0.01384000 -0.00008000 -0.01382000 -0.03805000 -0.07705000 12 0.08209000 0.03569000 -0.00657000 -0.00006000 0.00655000 -0.03566000 -0.08206000 15 0.06423000 0.03515000 0.01362000 -0.00152000 -0.01361000 -0.03505000 -0.06419000 17 0.05624000 0.02666000 0.01223000 0.00003000 -0.01213000 -0.02664000 -0.05615000 20 0.05028000 0.02335000 0.00637000 -0.00010000 -0.00613000 -0.02314000 -0.05025000 25 0.04074000 0.05032000 0.01422000 -0.00002000 -0.01299000 -0.02995000 -0.04067000 30 0.02733000 -0.00070000 0.02656000 0.00001000 -0.02447000 0.00059000 -0.02730000 45 0.01836000 -0.01916000 0.00510000 0.00007000 0.00976000 0.01932000 -0.01830000 50 -0.34624000 -0.01021000 -0.01270000 0.00005000 0.01267000 0.01042000 0.34421000 -10 -5 -2 0 2 5 10 -10 0.07473000 0.03872000 0.01576000 0.00000000 -0.01616000 -0.03907000 -0.07476000 -5 0.07796000 0.04194000 0.01773000 0.00000000 -0.01801000 -0.04210000 -0.07793000 -2 0.07544000 0.04377000 0.01859000 0.00000000 -0.01859000 -0.04377000 -0.07545000 0 0.07820000 0.04525000 0.01845000 0.00000000 -0.02002000 -0.04517000 -0.07820000 2 0.07611000 0.04500000 0.01757000 0.00001000 -0.01757000 -0.04500000 -0.07610000 5 0.06618000 0.04086000 0.01701000 -0.00002000 -0.01701000 -0.04086000 -0.06666000 7 0.03403000 0.04021000 0.01412000 -0.00012000 -0.01412000 -0.04009000 -0.03406000 10 0.07602000 0.03780000 0.01386000 -0.00009000 -0.01384000 -0.03780000 -0.07603000 12 0.08112000 0.03476000 -0.00579000 -0.00006000 0.00577000 -0.03473000 -0.08111000 15 0.06213000 0.03341000 0.01373000 -0.00007000 -0.01372000 -0.03345000 -0.06209000 17 0.05439000 0.02556000 0.01178000 0.00003000 -0.01175000 -0.02555000 -0.05435000 20 0.04918000 0.02294000 0.00629000 -0.00010000 -0.00628000 -0.02266000 -0.04912000 25 0.04055000 0.02918000 0.01406000 -0.00002000 -0.01272000 -0.02934000 -0.04049000 30 0.02856000 -0.00003000 0.02521000 -0.00002000 -0.02314000 -0.00008000 -0.02853000 45 0.02130000 -0.01874000 -0.00950000 0.00006000 0.00883000 0.01890000 -0.02124000 50 -0.34708000 -0.00978000 -0.01266000 0.00005000 0.01249000 0.00998000 0.35028000 SIDEFORCE INCREMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 7 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 12 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 15 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 17 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 20 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 25 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 30 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 45 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 0.00062000 0.00045000 0.00003000 0.00000000 -0.00028000 -0.00044000 -0.00062000 -5 0.00314000 0.00157000 0.00069000 0.00000000 -0.00069000 -0.00158000 -0.00344000 -2 0.00420000 0.00176000 0.00043000 0.00000000 -0.00057000 -0.00177000 -0.00488000 0 0.01159000 0.00148000 0.00053000 -0.00002000 -0.00054000 0.00039000 -0.00565000 2 0.00585000 0.00140000 -0.00007000 0.00000000 0.00006000 -0.00141000 -0.00606000 5 0.00841000 0.00153000 0.00057000 -0.00525000 -0.00057000 -0.00154000 -0.00709000 7 0.01341000 0.00088000 0.00156000 0.00002000 -0.00125000 -0.00088000 -0.01343000 10 0.00524000 0.00060000 0.00062000 0.00001000 -0.00063000 -0.00060000 -0.01571000 12 0.00170000 0.00188000 0.00189000 -0.00439000 -0.00189000 -0.00187000 -0.00182000 15 0.00586000 0.00157000 0.00018000 0.00000000 -0.00649000 -0.00157000 -0.00596000 17 0.00420000 0.00142000 0.00000000 0.00000000 0.00007000 -0.00142000 -0.00404000 20 0.00111000 0.00096000 0.00002000 0.00001000 -0.00003000 -0.00093000 -0.00112000 25 0.00113000 -0.00092000 -0.00884000 0.00000000 0.00132000 0.00092000 -0.00115000 30 0.00370000 0.00236000 -0.00072000 0.00000000 0.00060000 -0.00255000 -0.00411000 45 0.00905000 0.00488000 0.00213000 0.00000000 -0.00205000 -0.00357000 -0.00203000 50 -0.00032000 0.00364000 0.01565000 0.00000000 -0.00176000 -0.00371000 0.00032000 -10 -5 -2 0 2 5 10 -10 0.00234000 0.00148000 0.00051000 0.00000000 -0.00076000 -0.00147000 -0.00234000 -5 0.00992000 0.00472000 0.00209000 0.00000000 -0.00236000 -0.00473000 -0.00994000 -2 0.01286000 0.00550000 0.00169000 0.00000000 -0.00181000 -0.00552000 -0.01354000 0 0.01619000 0.00523000 0.00215000 -0.00003000 -0.00216000 -0.00523000 -0.01612000 2 0.01747000 0.00506000 0.00061000 0.00000000 -0.00062000 -0.00507000 -0.01768000 5 0.02682000 0.00569000 0.00217000 -0.00524000 -0.00217000 -0.00569000 -0.02682000 7 0.03262000 0.00313000 0.00345000 0.00005000 -0.00345000 -0.00313000 -0.03264000 10 0.01413000 0.00357000 0.00176000 0.00004000 -0.00177000 -0.00358000 -0.01399000 12 0.00417000 0.00339000 0.00398000 -0.00437000 -0.00398000 -0.00338000 -0.00442000 15 0.01176000 0.00250000 0.00000000 0.00001000 -0.00631000 -0.00249000 -0.01186000 17 0.00854000 0.00376000 -0.00043000 0.00000000 0.00003000 -0.00328000 -0.00841000 20 0.00423000 0.00238000 0.00031000 0.00002000 -0.00032000 -0.00237000 -0.00425000 25 0.00340000 -0.00147000 -0.00268000 -0.00009000 0.00255000 0.00149000 -0.00343000 30 0.00806000 0.00583000 -0.00159000 0.00001000 0.00127000 -0.00602000 -0.00970000 45 0.01863000 0.00752000 0.00426000 0.00000000 -0.00411000 -0.00751000 -0.01162000 50 0.00062000 0.00735000 0.01729000 -0.00001000 -0.00342000 -0.00735000 -0.00060000 -10 -5 -2 0 2 5 10 -10 0.00529000 0.00332000 0.00147000 0.00000000 -0.00145000 -0.00240000 -0.00529000 -5 0.01743000 0.00847000 0.00372000 0.00000000 -0.00863000 -0.00824000 -0.01749000 -2 0.02234000 0.00989000 0.00320000 0.00000000 -0.00332000 -0.00990000 -0.02317000 0 0.02588000 0.00833000 0.00368000 0.00500000 -0.00369000 -0.00843000 -0.02580000 2 0.02703000 0.00808000 0.00107000 0.00000000 -0.00108000 -0.00808000 -0.02724000 5 0.04166000 0.00809000 0.00311000 -0.00523000 -0.00311000 -0.00809000 -0.04167000 7 0.04908000 0.00424000 0.00601000 0.00008000 -0.00602000 -0.00376000 -0.04910000 10 0.02254000 0.00498000 0.00381000 0.00006000 -0.00382000 -0.00499000 -0.02247000 12 0.00300000 0.00267000 0.00544000 -0.00437000 -0.00544000 -0.00266000 -0.00324000 15 0.01550000 0.00322000 -0.00017000 0.00001000 -0.00934000 -0.00249000 -0.01560000 17 0.01228000 0.00503000 0.00022000 -0.00542000 -0.00016000 -0.00503000 -0.01213000 20 0.00670000 0.00348000 0.00064000 0.00003000 -0.00060000 -0.00348000 -0.00673000 25 0.00523000 -0.00171000 -0.00351000 0.00001000 0.00326000 0.00175000 -0.00528000 30 0.01326000 0.00842000 -0.00223000 0.00001000 0.00187000 -0.00841000 -0.01370000 45 0.02315000 0.00947000 0.00523000 0.00000000 -0.00514000 -0.00942000 -0.01613000 50 0.00223000 0.00868000 0.01779000 -0.00001000 -0.00392000 -0.00863000 -0.00221000 SIDE FORCE DUE TO ROLL RATE aero/pb aero/alpha-deg -10 0.08391860 -5 0.05570970 -2 0.04874830 0 0.01726700 2 0.06157040 5 0.08617030 7 0.27247570 10 0.23690150 12 0.36926930 15 0.30816260 17 0.03355240 20 0.31131560 25 0.25958090 30 0.41343290 45 0.15961840 50 0.01300980 SIDE FORCE DUE TO YAW RATE aero/rb aero/alpha-deg -10 -0.41328180 -5 -0.44547750 -2 -0.46285470 0 -0.50033340 2 -0.48127710 5 -0.50542530 7 -0.44899570 10 -0.49757990 12 -0.42241950 15 -0.43320530 17 -0.47946730 20 -0.44029680 25 -0.20408260 30 1.37738250 45 -0.24028330 50 -0.34905160 SIDE FORCE DUE TO AILERON DEFLECTION fcs/aileron-pos-deg aero/alpha-deg -10 0.00067520 -5 0.00104160 -2 0.00123680 0 0.00127280 2 0.00148320 5 0.00223200 7 0.00262160 10 0.00257760 12 0.00319040 15 0.00282080 17 0.00222640 20 0.00261200 25 0.00213120 30 0.00393920 45 0.00114240 50 0.00088320 SIDE FORCE DUE TO RUDDER DEFLECTION fcs/rudder-pos-deg aero/alpha-deg -10 0.00373767 -5 0.00455833 -2 0.00431667 0 0.00416000 2 0.00393933 5 0.00374700 7 0.00410700 10 0.00367867 12 0.00324933 15 0.00346567 17 0.00339833 20 0.00316900 25 0.00142500 30 0.00200867 45 0.00067267 50 0.00062067 BASIC YAWING MOMENT aero/alpha-degaero/beta-degfcs/elevator-pos-deg -10 -5 -2 0 2 5 10 -10 -0.02423000 -0.01245000 -0.00494000 0.00000000 0.00494000 0.01245000 0.02420000 -5 -0.02042000 -0.01093000 -0.00465000 0.00000000 0.00465000 0.01091000 0.02037000 -2 -0.01812000 -0.01024000 -0.00428000 0.00000000 0.00428000 0.01024000 0.01812000 0 -0.01862000 -0.01053000 -0.00389000 0.00000000 0.00389000 0.01055000 0.01862000 2 -0.01694000 -0.00979000 -0.00336000 0.00000000 0.00331000 0.00980000 0.01691000 5 -0.01642000 -0.00860000 -0.00365000 0.00001000 0.00365000 0.00860000 0.01639000 7 -0.00476000 -0.00868000 -0.00311000 0.00004000 0.00310000 0.00867000 0.00477000 10 -0.01818000 -0.00739000 -0.00221000 0.00002000 0.00220000 0.00739000 0.01819000 12 -0.02026000 -0.00777000 0.00567000 0.00004000 -0.00566000 0.00776000 0.02025000 15 -0.01878000 -0.01099000 -0.00116000 0.00003000 0.00116000 0.01098000 0.01878000 17 -0.01946000 -0.00936000 -0.00366000 -0.00001000 0.00366000 0.00936000 0.01946000 20 -0.02172000 -0.01094000 -0.00192000 0.00005000 0.00189000 0.01083000 0.02171000 25 -0.02370000 -0.01435000 -0.00095000 0.00001000 0.00038000 0.01449000 0.02367000 30 -0.02527000 -0.00483000 -0.01687000 0.00002000 0.01645000 0.00487000 0.02530000 45 -0.03197000 -0.00958000 -0.00534000 0.00000000 0.00529000 0.00965000 0.03200000 50 -0.03466000 -0.01517000 -0.00521000 0.00000000 0.00515000 0.01520000 -0.04205000 -10 -5 -2 0 2 5 10 -10 -0.02363000 -0.01215000 -0.00498000 0.00000000 0.00509000 0.01215000 0.02363000 -5 -0.02067000 -0.01110000 -0.00473000 0.00000000 0.00473000 0.01111000 0.02067000 -2 -0.01834000 -0.01046000 -0.00439000 0.00002000 0.00439000 0.01047000 0.01834000 0 -0.01812000 -0.01034000 -0.00426000 0.00000000 0.00403000 0.01034000 0.01812000 2 -0.01717000 -0.00999000 -0.00340000 0.00000000 0.00340000 0.01000000 0.01717000 5 -0.01586000 -0.00827000 -0.00371000 0.00003000 0.00375000 0.00827000 0.01586000 7 -0.00596000 -0.00869000 -0.00340000 0.00004000 0.00340000 0.00868000 0.00582000 10 -0.01799000 -0.00721000 -0.00247000 0.00002000 0.00247000 0.00720000 0.01800000 12 -0.02067000 -0.00803000 0.00585000 0.00004000 -0.00584000 0.00803000 0.02066000 15 -0.01847000 -0.01057000 -0.00153000 0.00003000 0.00153000 0.01056000 0.01847000 17 -0.02028000 -0.00973000 -0.00382000 -0.00001000 0.00382000 0.00973000 0.02028000 20 -0.02199000 -0.01120000 -0.00211000 0.00005000 0.00213000 0.01109000 0.02198000 25 -0.02491000 -0.01486000 0.00212000 0.00000000 0.00051000 0.01500000 0.02488000 30 -0.02604000 -0.00539000 -0.01651000 0.00002000 0.01609000 0.00544000 0.02607000 45 -0.03418000 -0.00987000 -0.00606000 0.00000000 0.00601000 0.00994000 0.03422000 50 0.04943000 -0.01602000 -0.00559000 0.00000000 0.00553000 0.01605000 -0.04893000 -10 -5 -2 0 2 5 10 -10 -0.02521000 -0.01268000 -0.00502000 0.00000000 0.00487000 0.01265000 0.02460000 -5 -0.02071000 -0.01126000 -0.00481000 0.00000000 0.00481000 0.01126000 0.02086000 -2 -0.01853000 -0.01072000 -0.00453000 0.00000000 0.00453000 0.01074000 0.01854000 0 -0.01928000 -0.01115000 -0.00418000 0.00000000 0.00418000 0.01115000 0.01928000 2 -0.01804000 -0.01040000 -0.00364000 -0.00090000 0.00364000 0.01023000 0.01752000 5 -0.01677000 -0.00909000 -0.00386000 0.00001000 0.00392000 0.00909000 0.01677000 7 -0.00573000 -0.00909000 -0.00345000 0.00004000 0.00345000 0.00907000 0.00575000 10 -0.01970000 -0.00833000 -0.00270000 0.00003000 0.00269000 0.00833000 0.01971000 12 -0.02135000 -0.00842000 0.00523000 0.00004000 -0.00522000 0.00842000 0.02134000 15 -0.02009000 -0.01120000 -0.00193000 0.00003000 0.00193000 0.01120000 0.02009000 17 -0.02128000 -0.01018000 -0.00402000 -0.00001000 0.00402000 0.01018000 0.02128000 20 -0.02405000 -0.01231000 -0.00238000 0.00006000 0.00239000 0.01220000 0.02405000 25 -0.02625000 -0.01544000 -0.00122000 0.00000000 0.00054000 0.01558000 0.02621000 30 -0.02844000 -0.00656000 -0.01620000 0.00001000 0.01580000 0.00647000 0.02848000 45 -0.03809000 -0.01062000 -0.00670000 0.00000000 0.00661000 0.01071000 0.03813000 50 0.05517000 -0.01679000 -0.00588000 0.00000000 0.00581000 0.01671000 -0.05510000 -10 -5 -2 0 2 5 10 -10 -0.02464000 -0.01274000 -0.00497000 0.00000000 0.00506000 0.01274000 0.02464000 -5 -0.02115000 -0.01150000 -0.00491000 0.00000000 0.00491000 0.01150000 0.02115000 -2 -0.01866000 -0.01112000 -0.00469000 0.00000000 0.00473000 0.01113000 0.01888000 0 -0.01984000 -0.01163000 -0.00441000 0.00001000 0.00441000 0.01163000 0.01981000 2 -0.01798000 -0.01091000 -0.00390000 0.00000000 0.00390000 0.01091000 0.01804000 5 -0.01709000 -0.00958000 -0.00410000 0.00143000 0.00410000 0.00958000 0.01709000 7 -0.00586000 -0.00955000 -0.00353000 0.00005000 0.00353000 0.00955000 0.00587000 10 -0.02077000 -0.00918000 -0.00296000 0.00002000 0.00296000 0.00918000 0.02077000 12 -0.02228000 -0.00890000 0.00458000 0.00946000 -0.00457000 0.00889000 0.02230000 15 -0.02100000 -0.01141000 -0.00236000 0.00003000 0.01643000 0.01141000 0.02099000 17 -0.02257000 -0.01070000 -0.00424000 -0.00001000 0.00422000 0.01070000 0.02242000 20 -0.02541000 -0.01309000 -0.00266000 0.00005000 0.00269000 0.01298000 0.02541000 25 -0.02766000 -0.01606000 -0.00138000 0.00000000 0.00083000 0.01620000 0.02763000 30 -0.02991000 -0.00726000 -0.01597000 0.00001000 0.01555000 0.00730000 0.03013000 45 -0.04081000 -0.01113000 -0.00720000 0.00000000 0.00712000 0.01119000 0.03923000 50 0.06041000 -0.01726000 -0.00865000 -0.00003000 0.00605000 0.01730000 -0.05992000 -10 -5 -2 0 2 5 10 -10 -0.02420000 -0.01250000 -0.00510000 0.00000000 0.00510000 0.01246000 0.02406000 -5 -0.02164000 -0.01182000 -0.00505000 0.00000000 0.00506000 0.01182000 0.02159000 -2 -0.01939000 -0.01159000 -0.00531000 0.00000000 0.00504000 0.01160000 0.01939000 0 -0.01968000 -0.01173000 -0.00468000 0.00000000 0.00468000 0.01173000 0.01968000 2 -0.01874000 -0.01152000 -0.00432000 0.00000000 0.00420000 0.01152000 0.01870000 5 -0.01680000 -0.00956000 -0.00432000 0.00001000 0.00432000 0.00968000 0.01680000 7 -0.00612000 -0.01010000 -0.00364000 0.00005000 0.00364000 0.01010000 0.00614000 10 -0.02100000 -0.00967000 -0.00326000 0.00003000 0.00325000 0.00966000 0.02101000 12 -0.02336000 -0.00944000 0.00391000 0.00003000 -0.00390000 0.00944000 0.02335000 15 -0.02113000 -0.01120000 -0.00281000 0.00162000 0.00281000 0.01129000 0.02113000 17 -0.02371000 -0.01128000 -0.00448000 -0.00001000 0.00446000 0.01128000 0.02365000 20 -0.02595000 -0.01348000 -0.00296000 0.00005000 0.00291000 0.01338000 0.02594000 25 -0.02910000 -0.02591000 -0.00150000 0.00000000 0.00101000 0.01683000 0.02905000 30 -0.03076000 -0.00781000 -0.01562000 0.00001000 0.01520000 0.00785000 0.03079000 45 -0.04192000 -0.01128000 0.02291000 0.00000000 0.00758000 0.01135000 0.04196000 50 0.06433000 -0.01778000 -0.00634000 -0.00004000 0.00627000 0.01782000 -0.06337000 -10 -5 -2 0 2 5 10 -10 -0.02523000 -0.01309000 -0.00518000 0.00000000 0.00533000 0.01323000 0.02523000 -5 -0.02231000 -0.01218000 -0.00523000 0.00000000 0.00533000 0.01223000 0.02229000 -2 -0.02006000 -0.01214000 -0.00521000 0.00000000 0.00521000 0.01214000 0.02006000 0 -0.02137000 -0.01288000 -0.00497000 0.00000000 0.00548000 0.01285000 0.02137000 2 -0.01957000 -0.01219000 -0.00452000 0.00000000 0.00452000 0.01219000 0.01956000 5 -0.01805000 -0.01078000 -0.00456000 0.00001000 0.00456000 0.01078000 0.01820000 7 -0.00655000 -0.01070000 -0.00378000 0.00005000 0.00378000 0.01068000 0.00657000 10 -0.02323000 -0.01108000 -0.00357000 0.00003000 0.00357000 0.01107000 0.02323000 12 -0.02448000 -0.01003000 0.00324000 0.00003000 -0.00323000 0.01002000 0.02447000 15 -0.02312000 -0.01200000 -0.00324000 0.00003000 0.00324000 0.01201000 0.02312000 17 -0.02489000 -0.01187000 -0.00472000 -0.00001000 0.00472000 0.01187000 0.02489000 20 -0.02821000 -0.01467000 -0.00326000 0.00005000 0.00328000 0.01456000 0.02819000 25 -0.03037000 -0.01727000 -0.00179000 0.00000000 0.00125000 0.01741000 0.03033000 30 -0.03310000 -0.00885000 -0.01553000 0.00002000 0.01511000 0.00889000 0.03313000 45 -0.04483000 -0.01190000 -0.00801000 0.00000000 0.00794000 0.01197000 0.04487000 50 0.06640000 -0.01818000 -0.00650000 -0.00004000 0.00643000 0.01822000 -0.06591000 YAWING MOMENT DUE TO AILERON DEFLECTION fcs/aileron-pos-deg aero/alpha-deg -10 0.00051680 -5 0.00031520 -2 0.00018720 0 0.00007920 2 0.00002080 5 0.00008480 7 0.00014640 10 -0.00003280 12 0.00079440 15 0.00008080 17 0.00004240 20 0.00046800 25 0.00023040 30 0.00149760 45 -0.00018160 50 -0.00020960 YAWING MOMENT DUE TO FLAPS aero/alpha-degaero/beta-degfcs/flap-pos-deg -10 -5 -2 0 2 5 10 -10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 2 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 5 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 7 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 10 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 12 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 15 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 17 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 20 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 25 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 30 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 45 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 50 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 -10 -5 -2 0 2 5 10 -10 0.00225000 0.00124000 0.00029000 0.00000000 -0.00038000 -0.00123000 -0.00224000 -5 0.00155000 0.00078000 0.00034000 0.00000000 -0.00034000 -0.00078000 -0.00165000 -2 0.00137000 0.00050000 0.00008000 0.00000000 -0.00012000 -0.00051000 -0.00159000 0 0.00426000 0.00061000 -0.00001000 -0.00001000 0.00001000 -0.00004000 -0.00231000 2 0.00103000 -0.00012000 -0.00035000 0.00000000 0.00035000 0.00012000 -0.00109000 5 0.00169000 0.00013000 -0.00020000 -0.00142000 0.00020000 -0.00014000 -0.00140000 7 0.00197000 -0.00070000 0.00003000 0.00000000 0.00001000 0.00070000 -0.00197000 10 -0.00069000 -0.00079000 -0.00033000 0.00001000 0.00032000 0.00079000 -0.01221000 12 -0.00339000 -0.00140000 -0.00038000 -0.00942000 0.00038000 0.00140000 0.00333000 15 -0.00316000 -0.00162000 -0.00092000 0.00000000 -0.01315000 0.00162000 0.00317000 17 -0.00253000 -0.00115000 -0.00056000 0.00000000 0.00058000 0.00115000 0.00268000 20 -0.00178000 -0.00093000 -0.00077000 0.00000000 0.00075000 0.00094000 0.00177000 25 -0.00272000 -0.00176000 -0.02349000 0.00000000 0.00111000 0.00176000 0.00272000 30 -0.00074000 -0.00053000 -0.00055000 0.00000000 0.00053000 0.00050000 0.00055000 45 0.00184000 0.00056000 0.00033000 0.00000000 -0.00031000 -0.00019000 -0.00023000 50 -0.00222000 0.00018000 0.00271000 0.00000000 -0.00018000 -0.00020000 0.00221000 -10 -5 -2 0 2 5 10 -10 0.00423000 0.00237000 0.00079000 0.00000000 -0.00088000 -0.00237000 -0.00422000 -5 0.00394000 0.00193000 0.00086000 0.00000000 -0.00095000 -0.00193000 -0.00394000 -2 0.00341000 0.00129000 0.00027000 0.00000000 -0.00031000 -0.00130000 -0.00363000 0 0.00441000 0.00100000 0.00014000 -0.00001000 -0.00014000 -0.00100000 -0.00438000 2 0.00277000 -0.00008000 -0.00073000 0.00000000 0.00073000 0.00008000 -0.00283000 5 0.00451000 -0.00003000 -0.00036000 -0.00141000 0.00036000 0.00003000 -0.00451000 7 0.00412000 -0.00145000 0.00013000 0.00002000 -0.00013000 0.00145000 -0.00412000 10 -0.00354000 -0.00097000 -0.00062000 0.00002000 0.00061000 0.00097000 0.00358000 12 -0.00659000 -0.00253000 -0.00058000 -0.00942000 0.00058000 0.00253000 0.00656000 15 -0.00462000 -0.00265000 -0.00142000 0.00001000 -0.01265000 0.00265000 0.00463000 17 -0.00460000 -0.00197000 -0.00117000 0.00000000 0.00106000 0.00210000 0.00467000 20 -0.00434000 -0.00220000 -0.00151000 0.00000000 0.00149000 0.00221000 0.00433000 25 -0.00536000 -0.00352000 -0.00223000 0.00013000 0.00224000 0.00352000 0.00535000 30 -0.00227000 -0.00109000 -0.00108000 0.00001000 0.00107000 0.00106000 0.00163000 45 0.00298000 0.00034000 0.00069000 0.00000000 -0.00066000 -0.00034000 -0.00136000 50 -0.00373000 0.00054000 0.00294000 0.00000000 -0.00040000 -0.00055000 0.00373000 -10 -5 -2 0 2 5 10 -10 0.00629000 0.00365000 0.00140000 0.00000000 -0.00138000 -0.00328000 -0.00628000 -5 0.00636000 0.00320000 0.00144000 0.00000000 -0.00490000 -0.00311000 -0.00638000 -2 0.00567000 0.00234000 0.00058000 0.00000000 -0.00062000 -0.00235000 -0.00594000 0 0.00659000 0.00147000 0.00041000 0.00188000 -0.00041000 -0.00151000 -0.00656000 2 0.00466000 0.00022000 -0.00095000 0.00000000 0.00095000 -0.00022000 -0.00471000 5 0.00747000 0.00012000 -0.00033000 -0.00141000 0.00033000 -0.00012000 -0.00747000 7 0.00675000 -0.00189000 0.00067000 0.00003000 -0.00067000 0.00211000 -0.00676000 10 -0.00442000 -0.00112000 -0.00052000 0.00003000 0.00051000 0.00111000 0.00444000 12 -0.00909000 -0.00360000 -0.00045000 -0.00942000 0.00045000 0.00361000 0.00906000 15 -0.00530000 -0.00328000 -0.00176000 0.00001000 -0.01276000 -0.01355000 0.00532000 17 -0.00549000 -0.00251000 -0.00129000 -0.00144000 0.00131000 0.00251000 0.00564000 20 -0.00590000 -0.00296000 -0.00194000 0.00001000 0.00193000 0.00297000 0.00589000 25 -0.00686000 -0.00457000 -0.00289000 0.00000000 0.00288000 0.00457000 0.00685000 30 -0.00212000 -0.00124000 -0.00137000 0.00001000 0.00131000 0.00123000 0.00194000 45 0.00392000 0.00065000 0.00093000 0.00000000 -0.00090000 -0.00063000 -0.00231000 50 -0.00342000 0.00092000 0.00310000 0.00000000 -0.00056000 -0.00092000 0.00341000 YAWING MOMENT DUE TO RUDDER DEFLECTION fcs/rudder-pos-deg aero/alpha-degaero/beta-deg -10 -5 -2 0 2 5 10 -10 -0.00227600 -0.00226133 -0.00221333 -0.00173333 -0.00220333 -0.00222100 -0.00219133 -5 -0.00212633 -0.00210167 -0.00209933 -0.00209700 -0.00208367 -0.00205833 -0.00203400 -2 -0.00205267 -0.00201500 -0.00198567 -0.00197500 -0.00196767 -0.00196733 -0.00193700 0 -0.00205533 -0.00200367 -0.00191467 -0.00193833 -0.00189467 -0.00194100 -0.00192000 2 -0.00196267 -0.00190367 -0.00184167 -0.00178633 -0.00181800 -0.00184033 -0.00181500 5 -0.00195600 -0.00189500 -0.00182000 -0.00176967 -0.00178833 -0.00180800 -0.00182533 7 -0.00148967 -0.00181700 -0.00180433 -0.00183833 -0.00177500 -0.00172333 -0.00158500 10 -0.00184167 -0.00181400 -0.00167100 -0.00167533 -0.00162433 -0.00168767 -0.00171100 12 -0.00166033 -0.00169000 -0.00184533 -0.00119067 -0.00148267 -0.00155900 -0.00154800 15 -0.00165800 -0.00167567 -0.00152367 -0.00153967 -0.00097167 -0.00152733 -0.00147533 17 -0.00152100 -0.00152000 -0.00147100 -0.00145467 -0.00138433 -0.00137067 -0.00136800 20 -0.00144167 -0.00141067 -0.00136000 -0.00136833 -0.00126433 -0.00125767 -0.00130900 25 -0.00123267 -0.00121567 -0.00130267 -0.00064367 -0.00120167 -0.00108933 -0.00111833 30 -0.00112833 -0.00114567 -0.00061967 -0.00145700 0.00002267 -0.00104267 -0.00100367 45 -0.00086233 -0.00044133 -0.00087433 -0.00023400 -0.00074733 -0.00031000 -0.00070500 50 0.00066333 -0.00169100 -0.00030833 -0.00025233 -0.00023333 -0.00038967 -0.00008267 YAWING MOMENT DUE TO ROLL RATE aero/pb aero/alpha-deg -10 -0.10099160 -5 -0.02302790 -2 0.01742970 0 0.05461480 2 0.05877090 5 0.09037420 7 0.04263890 10 0.10228660 12 0.04854240 15 0.09407840 17 0.16975820 20 0.01427700 25 0.07055640 30 -0.09428040 45 0.06385380 50 0.08125230 YAW DAMPING DERIVATIVE aero/rb aero/alpha-deg -10 -0.15850920 -5 -0.15940230 -2 -0.15959790 0 -0.17287060 2 -0.15608680 5 -0.16310810 7 -0.13286630 10 -0.15484240 12 -0.10580540 15 -0.13294470 17 -0.16899230 20 -0.17569740 25 -0.11818280 30 0.03448160 45 -0.09014590 50 -0.14338380 aero/coefficients/CFZB aero/coefficients/CFZDF aero/qbar-psf metrics/Sw-sqft aero/coefficients/CLIFT aero/coefficients/CFXB aero/coefficients/CFXDF aero/qbar-psf metrics/Sw-sqft aero/coefficients/CDRAG aero/coefficients/CFYB aero/coefficients/CFYP aero/coefficients/CFYR aero/coefficients/CYDAD aero/coefficients/CYDRD aero/coefficients/CFYDF aero/qbar-psf metrics/Sw-sqft aero/coefficients/CSIDE aero/coefficients/CML1 aero/coefficients/CMLP aero/coefficients/CMLR aero/coefficients/CMLDAD aero/coefficients/CMLDRD aero/coefficients/CMLDF aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/coefficients/CROLL aero/coefficients/CMM1 aero/coefficients/CMMQ aero/coefficients/CMMDF aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/coefficients/CPITCH aero/coefficients/CMN1 aero/coefficients/CMNDF aero/coefficients/CMNDRDr aero/coefficients/CMNP aero/coefficients/CMNR aero/coefficients/CMNDAD aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/coefficients/CYAW

ON ON ON ON ON ON ON ON ON