Ron Jensen, Erik Hofman, Aeromatic v 0.9
2008-07-26
$Revison: $
Models a Fokker Dr.1.
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.
201.31
23.62
2.00
8.52
32.21
9.84
20.13
9.47
0.00
0.00
0.00
29.53
-18.00
45.00
0
0
0
368.55
522.24
731.37
775
0.00
0.00
-5.68
-8.5
-30.59
-69.60
0.80
0.50
0.02
1000
500
0
NONE
0
-8.5
30.59
-69.60
0.80
0.50
0.02
1000
500
0
NONE
0
157.48
0.00
-26.85
0.80
0.50
0.02
200
100
0.00
NONE
0
22.4
-108.8
-34.8
0.80
0.50
300
150
22.4
108.8
-34.8
0.80
0.50
300
150
-25.00
0.00
0.00
0.00
0.00
0.00
0
-36.36
0.00
0.00
0.00
0.00
0.00
0.04
0.00
-5.68
100.00
50.00
-1
1
-0.35
0.35
fcs/elevator-pos-rad
-0.31
0.26
-1
1
fcs/elevator-pos-norm
-1
1
-0.30
0.30
fcs/left-aileron-pos-rad
-0.30
0.30
fcs/right-aileron-pos-rad
-0.30
0.30
-1
1
fcs/left-aileron-pos-norm
-0.30
0.30
-1
1
fcs/right-aileron-pos-norm
-0.35
0.35
-0.44
0.44
fcs/rudder-pos-rad
-0.44
0.44
-1
1
fcs/rudder-pos-norm
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-deg
-180.000000 0
-167.283800 0.507559
-165.091352 0.503240
-160.267966 0.460043
-158.075518 0.451404
-155.883069 0.460043
-150.182704 0.498920
-140.535932 0.498920
-124.311815 0.451404
-113.349574 0.356371
-103.702801 0.239741
-94.056029 0.084233
-85.000000 -0.053212
-83.000000 -0.075185
-79.000000 -0.119132
-75.000000 -0.163079
-71.000000 -0.207027
-67.000000 -0.250974
-63.000000 -0.294921
-59.000000 -0.330791
-55.000000 -0.362833
-51.000000 -0.394875
-49.000000 -0.410896
-45.000000 -0.442939
-43.000000 -0.458960
-41.000000 -0.474981
-39.000000 -0.492972
-35.000000 -0.530579
-31.000000 -0.568186
-29.000000 -0.586989
-27.000000 -0.605792
-25.000000 -0.620705
-23.000000 -0.633666
-21.000000 -0.619398
-19.000000 -0.593683
-17.000000 -0.562693
-15.000000 -0.531727
-13.000000 -0.506665
-11.000000 -0.430152
-9.000000 -0.305751
-7.000000 -0.181350
-5.000000 -0.056949
-3.000000 0.067354
-1.000000 0.191575
1.000000 0.315796
3.000000 0.440017
5.000000 0.564237
7.000000 0.689083
9.000000 0.814508
11.000000 0.927432
13.000000 1.016563
15.000000 1.074647
17.000000 1.044252
19.000000 0.916713
21.000000 0.742705
23.000000 0.655686
25.000000 0.615506
27.000000 0.592442
29.000000 0.569378
31.000000 0.552969
33.000000 0.542580
35.000000 0.532191
37.000000 0.521802
39.000000 0.511413
41.000000 0.499081
43.000000 0.486002
45.000000 0.472923
47.000000 0.459843
49.000000 0.446764
51.000000 0.433685
53.000000 0.420605
55.000000 0.406311
57.000000 0.388495
59.000000 0.370678
61.000000 0.352862
63.000000 0.335045
65.000000 0.317229
67.000000 0.299343
69.000000 0.276179
71.000000 0.253014
73.000000 0.229849
75.000000 0.206684
77.000000 0.183520
79.000000 0.160355
81.000000 0.135592
83.000000 0.105045
85.000000 0.074498
90.548112 0.002160
104.141291 -0.218143
122.119367 -0.399568
136.589525 -0.455724
150.621194 -0.451404
155.883069 -0.416847
157.637028 -0.412527
159.390987 -0.425486
163.775883 -0.455724
165.968331 -0.468683
167.722290 -0.447084
180.000000 0
Lift_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.2
Drag_at_zero_lift
aero/qbar-psf
metrics/Sw-sqft
0.0323
Induced_drag
aero/qbar-psf
metrics/Sw-sqft
aero/cl-squared
aero/alpha-deg
-180.000000 0.036717
-169.914738 0.062635
-150.182704 0.153348
-122.119367 0.265659
-84.847747 0.408207
-45.383678 0.533477
-43.000000 0.527482
-41.000000 0.530885
-39.000000 0.534288
-37.000000 0.528571
-35.000000 0.513248
-33.000000 0.497924
-31.000000 0.482600
-29.000000 0.467276
-27.000000 0.451953
-25.000000 0.416920
-23.000000 0.374764
-21.000000 0.332608
-19.000000 0.290452
-17.000000 0.238177
-15.000000 0.175336
-13.000000 0.085176
-11.000000 0.029907
-9.000000 0.002152
-7.000000 0.001623
-5.000000 0.001818
-3.000000 0.002013
-1.000000 0.002207
1.000000 0.002402
3.000000 0.002597
5.000000 0.002792
7.000000 0.002986
9.000000 0.003181
11.000000 0.003376
13.000000 0.013600
15.000000 0.032951
17.000000 0.060633
19.000000 0.092297
21.000000 0.123961
23.000000 0.157220
25.000000 0.200529
27.000000 0.243839
29.000000 0.287148
31.000000 0.330457
33.000000 0.364475
35.000000 0.398403
37.000000 0.432331
39.000000 0.466259
41.000000 0.500187
43.000000 0.533927
45.000000 0.551580
47.000000 0.569232
49.000000 0.586885
51.000000 0.604537
53.000000 0.622189
55.000000 0.638904
57.000000 0.645843
59.000000 0.652782
61.000000 0.655156
63.000000 0.645551
65.000000 0.635947
67.000000 0.625216
69.000000 0.603688
71.000000 0.582160
73.000000 0.560632
75.000000 0.539104
77.000000 0.508452
79.147381 0.481641
100.633374 0.334773
132.643118 0.192225
160.706456 0.079914
180.000000 0.036717
Drag_due_to_sideslip
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
Drag_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/mag-elevator-pos-rad
0.0136
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-0.3855
Side_force_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
fcs/rudder-pos-rad
0.094
Side_force_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/p-aero-rad_sec
-0.01
Side_force_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/r-aero-rad_sec
0.1047
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
-0.02
Roll_moment_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
-0.193
Roll_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
0.458
Roll_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.087
Roll_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
0.005
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-deg
-180.000000 0.002160
-155.444580 0.049676
-127.381242 0.088553
-84.847747 0.118790
-83.000000 0.111578
-81.000000 0.109529
-79.000000 0.107307
-77.000000 0.104574
-75.000000 0.101924
-73.000000 0.099422
-71.000000 0.097083
-69.000000 0.094282
-67.000000 0.091509
-65.000000 0.088937
-63.000000 0.086618
-61.000000 0.084993
-59.000000 0.084405
-57.000000 0.084065
-55.000000 0.083979
-53.000000 0.084150
-51.000000 0.084585
-49.000000 0.085133
-47.000000 0.084831
-45.000000 0.084135
-43.000000 0.083629
-41.000000 0.083319
-39.000000 0.082857
-37.000000 0.081386
-35.000000 0.078832
-33.000000 0.076293
-31.000000 0.073780
-29.000000 0.070542
-27.000000 0.066352
-25.000000 0.059782
-23.000000 0.052199
-21.000000 0.048019
-19.000000 0.036628
-17.000000 0.008613
-15.000000 -0.021966
-13.000000 -0.051723
-11.000000 -0.061373
-9.000000 -0.055043
-7.000000 -0.042039
-5.000000 -0.030525
-3.000000 -0.020684
-1.000000 -0.012551
1.000000 -0.006150
3.000000 -0.001511
5.000000 0.001345
7.000000 0.002421
9.000000 0.001690
11.000000 -0.001231
13.000000 -0.004202
15.000000 -0.006967
17.000000 -0.015326
19.000000 -0.039137
21.000000 -0.053761
23.000000 -0.057517
25.000000 -0.059092
27.000000 -0.059484
29.000000 -0.057321
31.000000 -0.055292
33.000000 -0.055424
35.000000 -0.055607
37.000000 -0.055193
39.000000 -0.054363
41.000000 -0.053475
43.000000 -0.052650
45.000000 -0.054951
47.000000 -0.057268
49.000000 -0.059612
51.000000 -0.061994
53.000000 -0.063932
55.000000 -0.065632
57.000000 -0.068524
59.000000 -0.071343
61.000000 -0.074801
63.000000 -0.079945
65.000000 -0.084862
67.000000 -0.089696
69.000000 -0.094872
71.000000 -0.099632
73.000000 -0.103974
75.000000 -0.107735
77.000000 -0.111800
79.000000 -0.115339
81.000000 -0.117895
83.000000 -0.116303
85.724726 -0.110151
121.680877 -0.079914
154.567600 -0.041037
180.000000 0.002160
Pitch_moment_due_to_elevator
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-deg
fcs/elevator-pos-rad
-0.35 0 0.35
-180.000 0.015374 0.000000 -0.015374
-163.145 0.100936 0.081551 0.065508
-161.555 0.105615 0.084893 0.063503
-159.965 0.103610 0.082219 0.057487
-157.420 0.096257 0.076203 0.052807
-155.512 0.092914 0.072193 0.056150
-153.604 0.100267 0.075535 0.080214
-146.608 0.129011 0.106283 0.121658
-137.703 0.162433 0.139706 0.145053
-124.028 0.187834 0.162433 0.154412
-104.947 0.194519 0.172460 0.155080
-91.227 0.195800 0.173500 0.153400
-71.329 0.193000 0.165200 0.130500
-53.688 0.186900 0.150800 0.105100
-41.556 0.180900 0.135600 0.071000
-34.678 0.176100 0.120200 0.076400
-30.176 0.173500 0.113200 0.088700
-25.540 0.176700 0.130300 0.084000
-22.669 0.171600 0.132500 0.064600
-16.566 0.151400 0.117400 0.015500
-1.000 0.098300 0.000400 -0.099000
6.800 0.042300 -0.040000 -0.136000
14.848 -0.015500 -0.117400 -0.151400
21.533 -0.064600 -0.132500 -0.171600
24.758 -0.084000 -0.130300 -0.176700
28.255 -0.088700 -0.113200 -0.173500
30.402 -0.076400 -0.120200 -0.176100
38.547 -0.071000 -0.135600 -0.180900
54.266 -0.105100 -0.150800 -0.186900
69.499 -0.130500 -0.165200 -0.193000
89.241 -0.153400 -0.173500 -0.195800
113.534 -0.154412 -0.172460 -0.194519
128.481 -0.145053 -0.162433 -0.187834
139.611 -0.121658 -0.139706 -0.162433
150.424 -0.080214 -0.106283 -0.129011
155.830 -0.056150 -0.075535 -0.100267
157.739 -0.052807 -0.072193 -0.092914
159.647 -0.057487 -0.076203 -0.096257
161.555 -0.063503 -0.082219 -0.103610
163.145 -0.065508 -0.084893 -0.105615
165.053 -0.059492 -0.081551 -0.100936
180.000 0.015374 0.000000 -0.015374
Pitch_moment_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-1.839
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-1.122
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
0.096
Yaw_moment_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
-0.0109
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-0.082
Yaw_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
-0.0502
Adverse_yaw
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.0552