Unknown 2002-01-01 $Id: c172p.xml,v 1.40 June 2015 $ Cessna C-172 174 35.8 4.9 21.9 15.7 16.5 0 47 0 59.4 37 0 48 42.6 0 38.5 948 1346 1967 -0 -0 -0 1500 41 0 36.5 180 36 -14 24 0 36 14 24 0 70 -14 24 0 70 14 24 0 95 0 24 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 41 -43 -25 0 41 43 -25 0 41 -43 -25 0 41 43 -25 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 7.75 0 26.6 0 -0.886 0.316 0.082 The hydrodynamic interactions of the floats are modelled by external forces. -6.8 0 -19.5 0.8 0.5 0.02 1800 600 10 NONE 0 58.2 -43 -15.5 0.8 0.5 0.02 5400 400 0.0 LEFT 0 58.2 43 -15.5 0.8 0.5 0.02 5400 400 0.0 RIGHT 0 226.7 0 17 0.5 0.25 2000 1000 20 -232 50 0.75 0.5 1830.15 366.03 20 232 50 0.75 0.5 1830.15 366.03 -6.8 0 0 0.9 0.5 1830.15 366.03 58.2 -48 0 0.8 0.4 1830.15 366.03 58.2 48 0 0.8 0.4 1830.15 366.03 -119 0 35 .75 .5 1830.15 366.03 -119 0 8 3.0 2.0 1830.15 366.03 -4.7 0 60 3.0 2.0 1830.15 366.03 253.5 0 90 3.0 2.0 1830.15 366.03 3.230 -56.889 38.5 0.6 0.5 10000.00 2500.00 3.230 56.889 38.5 0.6 0.5 10000.00 2500.00 70.16 -56.889 38.5 0.6 0.5 10000.00 2500.00 70.16 56.889 38.5 0.6 0.5 10000.00 2500.00 160.71 -56.889 38.5 0.6 0.5 10000.00 2500.00 160.71 56.889 38.5 0.6 0.5 10000.00 2500.00 -78 -56.889 0 0.80 0.50 0.02 1000 600 360 NONE 1 -78 56.889 0 0.80 0.50 0.02 1000 600 360 NONE 1 76 -56.889 0 0.80 0.50 0.02 5400 1600 0 LEFT 1 76 56.889 0 0.80 0.50 0.02 5400 1600 0 RIGHT 1 18.44 0 -10 0.8 0.5 0.02 1800 600 10 NONE 0 93 -51 -10 0.8 0.5 0.02 5400 400 0.0 NONE 0 93 52 -10 0.8 0.5 0.02 5400 400 0.0 NONE 0 -19.7 0 26.6 0.0 0 0 2 -37.7 0 26.6 0.0 0.0 0.0 1 5 -19.7 0 26.6 0.0 0 0 3 -37.7 0 26.6 0.0 0.0 0.0 1 5 56 -112 59.4 129.43 100.0 AVGAS 56 112 59.4 129.43 100.0 AVGAS 56 0 59.4 0.1 0.0 1 AVGAS 56 0 59.4 0.1 0.0 1 AVGAS fcs/elevator-cmd-norm -1 1 /sim/model/c172p/cockpit/yoke-elevator fcs/elevator-cmd-norm-filtered fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum 0.01745 -28 23 fcs/elevator-pos-rad fcs/elevator-pos-deg -28 23 -1 1 fcs/elevator-pos-norm fcs/aileron-cmd-norm -1 1 /sim/model/c172p/cockpit/yoke-aileron fcs/aileron-cmd-norm-filtered fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum 0.01745 -20 15 fcs/left-aileron-pos-rad fcs/left-aileron-pos-deg -20 15 -1 1 fcs/left-aileron-pos-norm fcs/roll-trim-sum -0.01745 -20 15 fcs/right-aileron-pos-rad fcs/right-aileron-pos-deg -15 20 1 -1 fcs/right-aileron-pos-norm fcs/rudder-cmd-norm -1 1 /sim/model/c172p/cockpit/pedals-rudder fcs/rudder-cmd-norm-filtered fcs/yaw-trim-cmd-norm -1 1 fcs/yaw-trim-sum 0.01745 -25 25 fcs/rudder-pos-rad fcs/rudder-pos-deg -25 25 -1 1 fcs/rudder-pos-norm fcs/flap-input-norm /systems/electrical/outputs/flaps le 16 fcs/flap-input-norm 0 10 20 30 fcs/flap-pos-deg fcs/flap-pos-deg 0 30 0 1 fcs/flap-pos-norm /controls/flight/flaps 0 1 /sim/model/c172p/cockpit/flaps-lever /controls/engines/engine/primer/controls/engines/current-engine/throttle 0.09 0.1 0.5 0.51 2 0 0 0 0 3 0 1 1 0 4 0 1 1 0 5 0 1 1 0 6 0 1 1 0 7 0 0 0 0
fcs/mixture-pos-norm[0] /controls/engines/engine/use-primer eq 1 /engines/engine[0]/oil-temperature-degf le 75 fcs/mixture-pos-norm[1] /controls/engines/engine/use-primer eq 1 /engines/engine[1]/oil-temperature-degf le 75 gear/gear-input-norm /systems/electrical/outputs/instrument-lights le 20.0 gear/gear-input-norm 0 1 gear/gear-pos-norm /controls/gear/water-rudder 0 1 -0.087 0.28 0.09 0.297 Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.4800 0.1000 0.5150 0.1500 0.6290 0.2000 0.7090 0.3000 0.8150 0.4000 0.8820 0.5000 0.9280 0.6000 0.9620 0.7000 0.9880 0.8000 1.0000 0.9000 1.0000 1.0000 1.0000 1.1000 1.0000
Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.2030 0.1000 1.1270 0.1500 1.0900 0.2000 1.0730 0.3000 1.0460 0.4000 1.0550 0.5000 1.0190 0.6000 1.0130 0.7000 1.0080 0.8000 1.0060 0.9000 1.0030 1.0000 1.0020 1.1000 1.0000
velocity including the propulsion induced velocity. velocities/u-aero-fps propulsion/engine/prop-induced-velocity_fps q bar including the propulsion induced velocity. aero/function/velocity-induced-fps aero/function/velocity-induced-fps atmosphere/rho-slugs_ft3 0.5 Total damage on wings wing-damage/left-wing wing-damage/right-wing 0.5 Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft 0.027 gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] Delta_drag_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCDge fcs/flap-pos-deg 0.0000 0.0000 10.0000 0.0070 20.0000 0.0120 30.0000 0.0180
Drag_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCDge aero/alpha-radfcs/flap-pos-deg 0 10 20 30 -0.0873 0.0041 0 0.0005 0.0014 -0.0698 0.0013 0.0004 0.0025 0.0041 -0.0524 0.0001 0.0023 0.0059 0.0084 -0.0349 0.0003 0.0057 0.0108 0.0141 -0.0175 0.002 0.0105 0.0172 0.0212 0.0000 0.0052 0.0168 0.0251 0.0299 0.0175 0.0099 0.0248 0.0346 0.0402 0.0349 0.0162 0.0342 0.0457 0.0521 0.0524 0.024 0.0452 0.0583 0.0655 0.0698 0.0334 0.0577 0.0724 0.0804 0.0873 0.0442 0.0718 0.0881 0.0968 0.1047 0.0566 0.0874 0.1053 0.1148 0.1222 0.0706 0.1045 0.124 0.1343 0.1396 0.086 0.1232 0.1442 0.1554 0.1571 0.0962 0.1353 0.1573 0.169 0.1745 0.1069 0.1479 0.1708 0.183 0.1920 0.118 0.161 0.1849 0.1975 0.2094 0.1298 0.1746 0.1995 0.2126 0.2269 0.1424 0.1892 0.2151 0.2286 0.2443 0.1565 0.2054 0.2323 0.2464 0.3491 0.2537 0.3298 0.3755 0.3983 0.5236 0.45 0.585 0.666 0.7065 0.6981 0.7 0.91 1.036 1.099 0.8727 1 1.3 1.48 1.57 1.0472 1.35 1.755 1.998 2.1195 1.2217 1.5 1.95 2.22 2.355 1.3963 1.57 2.041 2.3236 2.4649 1.5710 1.6 2.08 2.368 2.512
gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/mag-elevator-pos-rad 0.0000 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/mag-beta-rad 0.1500 gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-radfcs/flap-pos-deg 0.0000 30.0000 -0.3490 0.1370 0.1060 0.0000 0.0000 0.0000 0.3490 -0.1370 -0.1060
Side_force_due_to_rudder aero/qbar-psf metrics/Sw-sqft fcs/rudder-pos-rad 0.0374 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/alpha-radaero/stall-hyst-norm 0.00 1.00 -0.09 -0.22 -0.22 0.00 0.25 0.25 0.09 0.73 0.73 0.10 0.83 0.78 0.12 0.92 0.79 0.14 1.02 0.81 0.16 1.08 0.82 0.17 1.13 0.83 0.19 1.19 0.85 0.21 1.25 0.86 0.24 1.35 0.88 0.26 1.44 0.90 0.28 1.47 0.92 0.30 1.43 0.95 0.32 1.38 0.99 0.34 1.30 1.05 0.36 1.15 1.15 0.52 1.47 1.47 0.70 1.65 1.65 0.87 1.47 1.47 1.05 1.17 1.17 1.57 0.01 0.01
aero/function/total-wing-damage 0.0000 1 1.0000 0
Delta_lift_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/flap-pos-deg 0.0000 0.0000 10.0000 0.2000 20.0000 0.3000 30.0000 0.3500
Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.4300 Lift_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft aero/alphadot-rad_sec aero/ci2vel 1.7000 Lift_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft velocities/q-aero-rad_sec aero/ci2vel 3.9000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.3490 0.0322 0.0000 0.0000 0.3490 -0.0322 0.25
aero/alpha-wing-rad 0.279 1 0.297 3.5
Roll_moment_due_to_roll_rate_(roll_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -20 20 -10 9.68 -5 2.42 0 0 5 -2.42 10 -9.68 20 -20
Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec fcs/flap-pos-deg 0.0000 0.0798 30 0.1246
aero/alpha-wing-radvelocities/r-aero-rad_secaero/stall-hyst-norm -0.15 -0.1 0 0.1 0.15 0.279 1 1 1 1 1 0.297 35 30 1 30 35 0.5 5 5 1 5 5 -0.15 -0.1 0 0.1 0.15 0.297 35 30 1 30 35 0.5 5 5 1 5 5
Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.2290 aero/alpha-wing-radaero/stall-hyst-norm 0 1 0.279 1 0.3 0.297 0.3 0.3 0.611 -0.1 -0.1
aero/function/total-wing-damage 0.0000 1 1.0000 0
Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.0147 Roll_moment_due_to_damaged_left_wing aero/qbar-psf metrics/Sw-sqft metrics/bw-ft wing-damage/left-wing -0.3 Roll_moment_due_to_damaged_right_wing aero/qbar-psf metrics/Sw-sqft metrics/bw-ft wing-damage/right-wing 0.3 Pitching_moment_at_zero_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft 0.1000 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -1.8000 aero/alpha-deg 20 1 25 0.6 35 0.4 45 0.5 55 0.4 65 0.2 90 0.1
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -12.4000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -7.2700 Pitch_moment_due_to_elevator_deflection aero/function/qbar-induced-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad -1.8 aero/alpha-deg 18 1 25 0.5 35 0.2 45 0.1 55 0.1 65 0.1 90 0.1
Delta_pitching_moment_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/flap-pos-deg 0.0000 0.0000 10.0000 -0.0654 20.0000 -0.0981 30.0000 -0.1140
Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.3490 -0.0205 0.0000 0.0000 0.3490 0.0205
Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.0937 Yaw_moment_due_to_flat_spin aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_secaero/alpha-wing-rad 0.279 0.4 -15 0 0 -5 0 0 -3 0 -0.3 -1 0 0 0 0 0 1 0 0 3 0 0.3 5 0 0 15 0 0
Yaw_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad -0.016 aero/function/total-wing-damage 0.0000 1 1.0000 0
Yaw_moment_due_to_rudder aero/function/qbar-induced-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.07 32.6 0 38.5 1.0 0.0 0.0 32.6 0 38.5 0.0 1.0 0.0 32.6 0 38.5 0.0 0.0 -1.0 20.6 0 38.5 0.0 0.0 -1.0 44.6 0 38.5 0.0 0.0 -1.0 32.6 -12.0 38.5 1.0 0.0 0.0 32.6 12.0 38.5 1.0 0.0 0.0 32.6 -12.0 38.5 0.0 0.0 -1.0 32.6 12.0 38.5 0.0 0.0 -1.0 0.1188 -2.2998 0.4008 0.0 0.0 1.0 0.1188 2.2998 0.4008 0.0 0.0 1.0 4.7116 0.0000 -0.6663 0.0 0.0 1.0