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fgdata/Aircraft-uiuc/Pioneer-TD/Cmfade.dat
2000-10-22 21:05:31 +00:00

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1.9 KiB
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# Pioneer change in Cm as function of alpha and elevator deflection
-25
-6 0.9219
-4 0.8735
-2 0.827
0 0.7798
2 0.7413
4 0.6706
6 0.587
8 0.5293
10 0.4276
12 0.3045
13 0.2379
14 0.1698
15 0.1088
16 0.0503
17 -0.006
18 -0.0704
19 -0.1576
20 -0.2624
-20
-6 0.8532
-4 0.8031
-2 0.7546
0 0.7073
2 0.6698
4 0.5983
6 0.5275
8 0.4822
10 0.3743
12 0.252
13 0.1943
14 0.1367
15 0.0721
16 0.0109
17 -0.0452
18 -0.1072
19 -0.1668
20 -0.2034
-15
-6 0.7722
-4 0.7138
-2 0.6717
0 0.6258
2 0.5939
4 0.5384
6 0.4621
8 0.4109
10 0.3178
12 0.2058
13 0.1426
14 0.0705
15 0.0028
16 -0.0594
17 -0.123
18 -0.1827
19 -0.2384
20 -0.2822
-10
-6 0.6464
-4 0.5998
-2 0.559
0 0.5156
2 0.4682
4 0.4039
6 0.3265
8 0.2551
10 0.1513
12 0.0404
13 -0.0216
14 -0.0911
15 -0.1512
16 -0.2198
17 -0.2834
18 -0.3425
19 -0.3938
20 -0.4234
-5
-6 0.5099
-4 0.4673
-2 0.4248
0 0.3705
2 0.3111
4 0.2426
6 0.1675
8 0.0901
10 -0.0115
12 -0.1199
13 -0.1775
14 -0.2419
15 -0.3048
16 -0.3693
17 -0.429
18 -0.4869
19 -0.5246
20 -0.5369
0
-6 0.3524
-4 0.305
-2 0.2505
0 0.1922
2 0.1331
4 0.0681
6 -0.0041
8 -0.0826
10 -0.1771
12 -0.285
13 -0.3435
14 -0.4058
15 -0.4655
16 -0.5284
17 -0.583
18 -0.626
19 -0.6414
20 -0.6366
5
-6 0.2042
-4 0.1561
-2 0.1051
0 0.0403
2 -0.0198
4 -0.0833
6 -0.1556
8 -0.2472
10 -0.3376
12 -0.4361
13 -0.4882
14 -0.5455
15 -0.6097
16 -0.6657
17 -0.7117
18 -0.7409
19 -0.7367
20 -0.726
10
-6 0.0376
-4 -0.0146
-2 -0.075
0 -0.1391
2 -0.1921
4 -0.2594
6 -0.3327
8 -0.4179
10 -0.5038
12 -0.5937
13 -0.6446
14 -0.7024
15 -0.7536
16 -0.8052
17 -0.8406
18 -0.8481
19 -0.832
20 -0.8175
15
-6 -0.11
-4 -0.1606
-2 -0.2137
0 -0.2678
2 -0.3162
4 -0.378
6 -0.4518
8 -0.5384
10 -0.6162
12 -0.6994
13 -0.7465
14 -0.8015
15 -0.8507
16 -0.903
17 -0.9229
18 -0.9051
19 -0.8863
20 -0.8832
20
-6 -0.1353
-4 -0.1817
-2 -0.2356
0 -0.3001
2 -0.3675
4 -0.4532
6 -0.5296
8 -0.6121
10 -0.6925
12 -0.7772
13 -0.8266
14 -0.8897
15 -0.9399
16 -0.9818
17 -0.9877
18 -0.9575
19 -0.9439
20 -0.9447