Unknown
2002-01-01
$Id: c182.xml,v 1.24 2012/12/22 15:22:21 jberndt Exp $
Cessna C-182
This model was created using publicly available data, publicly available
technical reports, textbooks, and guesses. It contains no proprietary or
restricted data. If this model has been validated at all, it would be
only to the extent that it seems to "fly right", and that it possibly
complies with published, publicly known, performance data (maximum speed,
endurance, etc.). Thus, this model is meant for educational and entertainment
purposes only.
This simulation model is not endorsed by the manufacturer. This model is not
to be sold.
174
35.8
4.9
21.9
15.7
16.5
0
43.2
0
59.4
37
0
48
43.9
0
40.6
948
1346
1967
1700
41
0
36.5
180
36
-14
24
-6.8
0
-20
0.8
0.5
0.02
1800
600
10
NONE
0
58.2
-43
-17.9
0.8
0.5
0.02
5400
1600
360.0
LEFT
0
58.2
43
-17.9
0.8
0.5
0.02
5400
1600
360.0
RIGHT
0
188
0
8
0.2
0.2
0.2
20000
1000
0.0
NONE
0
43.2
-214.8
59.4
0.2
0.2
0.2
10000
2000
0.0
NONE
0
43.2
214.8
59.4
0.2
0.2
0.2
10000
2000
0.0
NONE
0
-19.7
0
26.6
0.0
0
0
0
1
-37.7
0
26.6
0.0
0.0
0.0
1
10
56
-112
59.4
300
200
56
112
59.4
300
200
-1
1
0.01745
-28
23
fcs/elevator-pos-rad
-25
35
-1
1
fcs/elevator-pos-norm
-1
1
0.01745
-20
15
fcs/left-aileron-pos-rad
-20
15
-0.75
1
fcs/left-aileron-pos-norm
-20
15
-0.75
1
fcs/right-aileron-pos-norm
-1
1
0.01745
-16
16
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
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
Drag_at_zero_lift
aero/qbar-psf
metrics/Sw-sqft
0.027
Drag_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
-0.0873 0.0041
-0.0698 0.0013
-0.0524 0.0001
-0.0349 0.0003
-0.0175 0.0020
0.0000 0.0052
0.0175 0.0099
0.0349 0.0162
0.0524 0.0240
0.0698 0.0334
0.0873 0.0442
0.1047 0.0566
0.1222 0.0706
0.1396 0.0860
0.1571 0.0962
0.1745 0.1069
0.1920 0.1180
0.2094 0.1298
0.2269 0.1424
0.2443 0.1565
0.2618 0.1727
0.2793 0.1782
0.2967 0.1716
0.3142 0.1618
0.3316 0.1475
0.3491 0.1097
Drag_due_to_sideslip
aero/qbar-psf
metrics/Sw-sqft
aero/mag-beta-rad
0.1700
Drag_due_to_flap_deflection
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
fcs/flap-pos-deg
0.0000 10.0000 20.0000 30.0000
-0.0873 0.0000 0.0030 0.0084 0.0153
-0.0698 0.0000 0.0061 0.0131 0.0208
-0.0524 0.0000 0.0092 0.0178 0.0263
-0.0349 0.0000 0.0124 0.0225 0.0317
-0.0175 0.0000 0.0155 0.0272 0.0372
0.0000 0.0000 0.0186 0.0319 0.0427
0.0175 0.0000 0.0218 0.0367 0.0483
0.0349 0.0000 0.0250 0.0415 0.0539
0.0524 0.0000 0.0282 0.0463 0.0594
0.0698 0.0000 0.0314 0.0511 0.0650
0.0873 0.0000 0.0346 0.0558 0.0706
0.1047 0.0000 0.0378 0.0606 0.0762
0.1222 0.0000 0.0409 0.0654 0.0818
0.1396 0.0000 0.0441 0.0702 0.0873
0.1571 0.0000 0.0461 0.0731 0.0907
0.1745 0.0000 0.0480 0.0760 0.0941
0.1920 0.0000 0.0499 0.0789 0.0975
0.2094 0.0000 0.0518 0.0818 0.1008
0.2269 0.0000 0.0538 0.0847 0.1043
0.2443 0.0000 0.0559 0.0879 0.1080
0.2618 0.0000 0.0582 0.0913 0.1120
0.2793 0.0000 0.0590 0.0925 0.1133
0.2967 0.0000 0.0581 0.0911 0.1117
0.3142 0.0000 0.0567 0.0890 0.1093
0.3316 0.0000 0.0546 0.0859 0.1056
0.3491 0.0000 0.0485 0.0767 0.0950
Drag_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/mag-elevator-pos-rad
0.0000
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
aero/alpha-rad
0.0000 -0.3930
0.0943 -0.4040
Side_force_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/p-aero-rad_sec
aero/alpha-rad
0.0000 -0.0750
0.0943 -0.1450
Side_force_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/r-aero-rad_sec
aero/alpha-rad
0.0000 0.2140
0.0943 0.2670
Side_force_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
fcs/left-aileron-pos-rad
0.0000
Side_force_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
fcs/rudder-pos-rad
0.1870
Lift_at_zero_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/function/kCLge
0.3070
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/function/kCLge
aero/alpha-rad
-0.0900 -0.5270
0.0000 -0.0570
0.1400 0.7130
0.2100 0.9450
0.2400 1.0470
0.2600 1.1330
0.2800 1.1590
0.3000 1.1250
0.3200 1.0740
0.3400 0.9910
0.3600 0.6630
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_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
Lift_due_to_elevator_deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.4300
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
aero/alpha-rad
0.0000 0.0943
-0.3490 0.0322 0.0312
0.0000 0.0000 0.0000
0.3490 -0.0322 -0.0312
Roll_moment_due_to_roll_rate_(roll_damping)
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
aero/alpha-rad
0.0000 -0.4840
0.0943 -0.4870
Roll_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
aero/alpha-rad
0.0000 0.0798
0.0943 0.1869
Roll_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.15
Roll_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
-0.0147
Pitching_moment_at_zero_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
0.0400
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
aero/alpha-rad
0.0000 -0.6130
0.0943 -0.6500
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
aero/alpha-rad
0.0000 -7.2700
0.0943 -5.5700
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_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
Pitch_moment_due_to_elevator_deflection
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/elevator-pos-rad
aero/alpha-rad
0.0000 -0.6220
0.0943 -0.8690
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
aero/alpha-rad
0.0000 0.0587
0.0943 0.0907
Yaw_moment_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
aero/alpha-rad
0.0000 -0.0278
0.0943 -0.0649
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
aero/alpha-rad
0.0000 -0.0937
0.0943 -0.1199
Yaw_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
aero/alpha-rad
0.0000 -0.0216
0.0943 -0.0504
Yaw_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
aero/alpha-rad
0.0000 -0.0645
0.0943 -0.0805