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
7.75
0
26.6
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
8
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
-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
185
100
56
112
59.4
185
100
56
0
59.4
0.1
0
1
56
0
59.4
0.1
0
1
-1
1
0.01745
-28
23
fcs/elevator-pos-rad
-28
23
-1
1
fcs/elevator-pos-norm
-1
1
0.01745
-20
15
fcs/left-aileron-pos-rad
-20
15
-1
1
fcs/left-aileron-pos-norm
-0.01745
-20
15
fcs/right-aileron-pos-rad
-15
20
1
-1
fcs/right-aileron-pos-norm
-1
1
0.01745
-25
25
fcs/rudder-pos-rad
-25
25
-1
1
fcs/rudder-pos-norm
0
0
10
2
20
1
30
1
fcs/flap-pos-deg
0
30
0
1
fcs/flap-pos-norm
/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
0
0
1
5
gear/gear-pos-norm
0
0
1
5
-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]
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-rad
fcs/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]
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]
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
fcs/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-rad
aero/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-rad
velocities/r-aero-rad_sec
aero/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-rad
aero/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_sec
aero/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