The 'PolarBrowser' application, a polar file converter is available
in the software section at:
http://www.MH-AeroTools.de/airfoils/
MH 42
xfoil 5.4 results: free transition
Copyright 2000-2004 Martin Hepperle
polar
60000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.125
0.01562
-0.0222
1.000
1.000
-99.999
-99.999
-2.000
-0.125
0.01562
-0.0222
1.000
1.000
-99.999
-99.999
-2.000
-0.125
0.01562
-0.0222
1.000
1.000
-99.999
-99.999
-1.500
-0.046
0.01602
-0.0299
0.967
1.000
-99.999
-99.999
-1.000
0.039
0.01659
-0.0374
0.931
1.000
-99.999
-99.999
-0.500
0.121
0.01716
-0.0439
0.899
1.000
-99.999
-99.999
0.000
0.191
0.01784
-0.0472
0.864
1.000
-99.999
-99.999
0.500
0.256
0.01842
-0.0494
0.833
1.000
-99.999
-99.999
1.000
0.316
0.01902
-0.0503
0.802
1.000
-99.999
-99.999
1.500
0.373
0.01964
-0.0503
0.771
1.000
-99.999
-99.999
2.000
0.428
0.02022
-0.0497
0.742
1.000
-99.999
-99.999
2.500
0.479
0.02080
-0.0483
0.711
1.000
-99.999
-99.999
3.000
0.530
0.02139
-0.0466
0.680
1.000
-99.999
-99.999
3.500
0.581
0.02188
-0.0444
0.650
1.000
-99.999
-99.999
4.000
0.630
0.02222
-0.0416
0.616
1.000
-99.999
-99.999
4.500
0.680
0.02247
-0.0386
0.580
1.000
-99.999
-99.999
5.000
0.729
0.02246
-0.0349
0.541
1.000
-99.999
-99.999
5.500
0.777
0.02205
-0.0304
0.490
1.000
-99.999
-99.999
6.000
0.823
0.02194
-0.0260
0.425
1.000
-99.999
-99.999
6.500
0.861
0.02271
-0.0217
0.333
1.000
-99.999
-99.999
7.000
0.891
0.02479
-0.0183
0.222
1.000
-99.999
-99.999
7.500
0.919
0.02833
-0.0158
0.131
1.000
-99.999
-99.999
8.000
0.949
0.03260
-0.0133
0.075
1.000
-99.999
-99.999
8.500
0.986
0.03746
-0.0109
0.048
1.000
-99.999
-99.999
9.000
1.021
0.04290
-0.0090
0.033
1.000
-99.999
-99.999
9.500
1.047
0.05046
-0.0071
0.025
1.000
-99.999
-99.999
10.000
1.056
0.05843
-0.0058
0.022
1.000
-99.999
-99.999
10.500
1.041
0.06784
-0.0055
0.020
1.000
-99.999
-99.999
11.000
1.003
0.07874
-0.0091
0.020
1.000
-99.999
-99.999
11.500
0.944
0.09610
-0.0226
0.022
1.000
-99.999
-99.999
12.000
0.884
0.12609
-0.0459
0.025
1.000
-99.999
-99.999
polar
100000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.070
0.01265
-0.0325
0.921
0.893
-99.999
-99.999
-1.500
0.077
0.01246
-0.0492
0.921
1.000
-99.999
-99.999
-1.000
0.141
0.01258
-0.0516
0.886
1.000
-99.999
-99.999
-0.500
0.195
0.01276
-0.0514
0.853
1.000
-99.999
-99.999
0.000
0.242
0.01300
-0.0493
0.822
1.000
-99.999
-99.999
0.500
0.287
0.01323
-0.0467
0.792
1.000
-99.999
-99.999
1.000
0.333
0.01350
-0.0444
0.764
1.000
-99.999
-99.999
1.500
0.381
0.01378
-0.0422
0.738
1.000
-99.999
-99.999
2.000
0.429
0.01407
-0.0403
0.711
1.000
-99.999
-99.999
2.500
0.478
0.01431
-0.0381
0.683
1.000
-99.999
-99.999
3.000
0.528
0.01460
-0.0363
0.654
1.000
-99.999
-99.999
3.500
0.578
0.01487
-0.0345
0.624
1.000
-99.999
-99.999
4.000
0.628
0.01504
-0.0323
0.590
1.000
-99.999
-99.999
4.500
0.678
0.01526
-0.0304
0.552
1.000
-99.999
-99.999
5.000
0.727
0.01550
-0.0283
0.505
1.000
-99.999
-99.999
5.500
0.775
0.01589
-0.0261
0.444
1.000
-99.999
-99.999
6.000
0.820
0.01669
-0.0239
0.362
1.000
-99.999
-99.999
6.500
0.861
0.01826
-0.0221
0.256
1.000
-99.999
-99.999
7.000
0.900
0.02063
-0.0206
0.143
1.000
-99.999
-99.999
7.500
0.935
0.02384
-0.0184
0.072
1.000
-99.999
-99.999
8.000
0.967
0.02754
-0.0157
0.040
1.000
-99.999
-99.999
8.500
1.002
0.03174
-0.0130
0.026
1.000
-99.999
-99.999
9.000
1.036
0.03717
-0.0105
0.018
1.000
-99.999
-99.999
9.500
1.064
0.04208
-0.0086
0.014
1.000
-99.999
-99.999
10.000
1.077
0.05007
-0.0063
0.011
1.000
-99.999
-99.999
10.500
1.076
0.05788
-0.0047
0.009
1.000
-99.999
-99.999
11.000
1.052
0.06649
-0.0045
0.009
1.000
-99.999
-99.999
11.500
1.014
0.07796
-0.0100
0.009
1.000
-99.999
-99.999
12.000
0.960
0.09576
-0.0242
0.010
1.000
-99.999
-99.999
polar
200000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.045
0.00926
-0.0342
0.854
0.686
-99.999
-99.999
-1.500
-0.005
0.00875
-0.0290
0.829
0.856
-99.999
-99.999
-1.000
0.065
0.00871
-0.0300
0.807
0.961
-99.999
-99.999
-0.500
0.165
0.00866
-0.0388
0.785
1.000
-99.999
-99.999
0.000
0.212
0.00876
-0.0372
0.759
1.000
-99.999
-99.999
0.500
0.260
0.00889
-0.0356
0.733
1.000
-99.999
-99.999
1.000
0.310
0.00906
-0.0343
0.709
1.000
-99.999
-99.999
1.500
0.360
0.00925
-0.0330
0.684
1.000
-99.999
-99.999
2.000
0.411
0.00943
-0.0319
0.658
1.000
-99.999
-99.999
2.500
0.463
0.00966
-0.0308
0.631
1.000
-99.999
-99.999
3.000
0.515
0.00989
-0.0299
0.602
1.000
-99.999
-99.999
3.500
0.567
0.01014
-0.0289
0.567
1.000
-99.999
-99.999
4.000
0.619
0.01045
-0.0280
0.529
1.000
-99.999
-99.999
4.500
0.670
0.01087
-0.0270
0.482
1.000
-99.999
-99.999
5.000
0.721
0.01142
-0.0261
0.423
1.000
-99.999
-99.999
5.500
0.770
0.01222
-0.0252
0.348
1.000
-99.999
-99.999
6.000
0.817
0.01338
-0.0244
0.256
1.000
-99.999
-99.999
6.500
0.863
0.01494
-0.0236
0.156
1.000
-99.999
-99.999
7.000
0.907
0.01683
-0.0225
0.076
1.000
-99.999
-99.999
7.500
0.949
0.01914
-0.0209
0.036
1.000
-99.999
-99.999
8.000
0.982
0.02244
-0.0183
0.019
1.000
-99.999
-99.999
8.500
1.015
0.02572
-0.0158
0.012
1.000
-99.999
-99.999
9.000
1.048
0.02913
-0.0135
0.007
1.000
-99.999
-99.999
9.500
1.075
0.03412
-0.0108
0.005
1.000
-99.999
-99.999
10.000
1.096
0.03942
-0.0084
0.004
1.000
-99.999
-99.999
10.500
1.100
0.04698
-0.0053
0.003
1.000
-99.999
-99.999
11.000
1.085
0.05545
-0.0036
0.003
1.000
-99.999
-99.999
11.500
1.057
0.06520
-0.0059
0.003
1.000
-99.999
-99.999
12.000
1.023
0.07718
-0.0131
0.003
1.000
-99.999
-99.999
12.500
0.983
0.09287
-0.0259
0.003
1.000
-99.999
-99.999
polar
400000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.056
0.00807
-0.0287
0.788
0.427
-99.999
-99.999
-1.500
-0.006
0.00735
-0.0275
0.765
0.614
-99.999
-99.999
-1.000
0.042
0.00672
-0.0253
0.742
0.796
-99.999
-99.999
-0.500
0.088
0.00642
-0.0222
0.720
0.916
-99.999
-99.999
0.000
0.163
0.00648
-0.0256
0.698
0.982
-99.999
-99.999
0.500
0.252
0.00657
-0.0326
0.673
1.000
-99.999
-99.999
1.000
0.302
0.00671
-0.0316
0.649
1.000
-99.999
-99.999
1.500
0.353
0.00685
-0.0307
0.625
1.000
-99.999
-99.999
2.000
0.404
0.00704
-0.0297
0.597
1.000
-99.999
-99.999
2.500
0.456
0.00724
-0.0289
0.569
1.000
-99.999
-99.999
3.000
0.509
0.00750
-0.0283
0.537
1.000
-99.999
-99.999
3.500
0.562
0.00781
-0.0277
0.500
1.000
-99.999
-99.999
4.000
0.614
0.00819
-0.0272
0.456
1.000
-99.999
-99.999
4.500
0.666
0.00870
-0.0267
0.402
1.000
-99.999
-99.999
5.000
0.718
0.00941
-0.0262
0.334
1.000
-99.999
-99.999
5.500
0.768
0.01032
-0.0258
0.256
1.000
-99.999
-99.999
6.000
0.817
0.01146
-0.0254
0.171
1.000
-99.999
-99.999
6.500
0.865
0.01279
-0.0248
0.093
1.000
-99.999
-99.999
7.000
0.912
0.01421
-0.0241
0.039
1.000
-99.999
-99.999
7.500
0.957
0.01596
-0.0228
0.018
1.000
-99.999
-99.999
8.000
0.999
0.01805
-0.0212
0.008
1.000
-99.999
-99.999
9.000
1.065
0.02415
-0.0164
0.002
1.000
-99.999
-99.999
9.500
1.094
0.02779
-0.0137
0.002
1.000
-99.999
-99.999
10.000
1.116
0.03240
-0.0109
0.002
1.000
-99.999
-99.999
10.500
1.126
0.03802
-0.0073
0.001
1.000
-99.999
-99.999
11.000
1.122
0.04486
-0.0047
0.001
1.000
-99.999
-99.999
11.500
1.105
0.05318
-0.0048
0.001
1.000
-99.999
-99.999
12.000
1.078
0.06337
-0.0087
0.001
1.000
-99.999
-99.999
12.500
1.044
0.07627
-0.0172
0.001
1.000
-99.999
-99.999
13.000
1.006
0.09325
-0.0307
0.001
1.000
-99.999
-99.999
polar
600000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.059
0.00768
-0.0269
0.751
0.298
-99.999
-99.999
-1.500
-0.007
0.00692
-0.0265
0.729
0.491
-99.999
-99.999
-1.000
0.045
0.00634
-0.0258
0.707
0.659
-99.999
-99.999
-0.500
0.096
0.00590
-0.0244
0.685
0.801
-99.999
-99.999
0.000
0.144
0.00563
-0.0221
0.664
0.910
-99.999
-99.999
0.500
0.209
0.00565
-0.0235
0.642
0.982
-99.999
-99.999
1.000
0.298
0.00578
-0.0308
0.615
0.999
-99.999
-99.999
1.500
0.352
0.00593
-0.0305
0.590
1.000
-99.999
-99.999
2.000
0.404
0.00612
-0.0296
0.561
1.000
-99.999
-99.999
2.500
0.455
0.00633
-0.0288
0.531
1.000
-99.999
-99.999
3.000
0.508
0.00660
-0.0282
0.496
1.000
-99.999
-99.999
3.500
0.560
0.00693
-0.0277
0.456
1.000
-99.999
-99.999
4.000
0.613
0.00736
-0.0272
0.406
1.000
-99.999
-99.999
4.500
0.665
0.00792
-0.0269
0.347
1.000
-99.999
-99.999
5.000
0.718
0.00856
-0.0266
0.288
1.000
-99.999
-99.999
5.500
0.768
0.00955
-0.0262
0.202
1.000
-99.999
-99.999
6.000
0.817
0.01076
-0.0258
0.116
1.000
-99.999
-99.999
6.500
0.867
0.01188
-0.0253
0.059
1.000
-99.999
-99.999
7.000
0.916
0.01298
-0.0248
0.027
1.000
-99.999
-99.999
7.500
0.962
0.01457
-0.0236
0.011
1.000
-99.999
-99.999
8.000
1.005
0.01655
-0.0222
0.003
1.000
-99.999
-99.999
8.500
1.047
0.01851
-0.0207
0.002
1.000
-99.999
-99.999
9.000
1.081
0.02130
-0.0184
0.001
1.000
-99.999
-99.999
9.500
1.107
0.02518
-0.0152
0.001
1.000
-99.999
-99.999
10.000
1.127
0.03027
-0.0118
0.001
1.000
-99.999
-99.999
10.500
1.136
0.03640
-0.0079
0.001
1.000
-99.999
-99.999
11.000
1.130
0.04348
-0.0049
0.001
1.000
-99.999
-99.999
11.500
1.112
0.05184
-0.0047
0.001
1.000
-99.999
-99.999
12.000
1.085
0.06190
-0.0083
0.001
1.000
-99.999
-99.999
12.500
1.051
0.07452
-0.0166
0.001
1.000
-99.999
-99.999
13.000
1.014
0.09080
-0.0296
0.001
1.000
-99.999
-99.999
xfoil 5.4 results: t.u. at 50%
Copyright 2000-2004 Martin Hepperle
polar
60000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
0.166
0.01920
-0.0590
0.500
0.878
-99.999
-99.999
-1.500
0.254
0.01859
-0.0658
0.500
0.920
-99.999
-99.999
-1.000
0.325
0.01795
-0.0702
0.500
0.953
-99.999
-99.999
-0.500
0.387
0.01744
-0.0730
0.500
0.979
-99.999
-99.999
0.000
0.438
0.01712
-0.0736
0.500
0.995
-99.999
-99.999
0.500
0.475
0.01699
-0.0717
0.500
1.000
-99.999
-99.999
1.000
0.510
0.01704
-0.0688
0.500
1.000
-99.999
-99.999
1.500
0.546
0.01714
-0.0662
0.500
1.000
-99.999
-99.999
2.000
0.585
0.01730
-0.0637
0.500
1.000
-99.999
-99.999
2.500
0.627
0.01754
-0.0616
0.500
1.000
-99.999
-99.999
3.000
0.670
0.01787
-0.0599
0.500
1.000
-99.999
-99.999
3.500
0.718
0.01833
-0.0588
0.500
1.000
-99.999
-99.999
4.000
0.772
0.01899
-0.0587
0.500
1.000
-99.999
-99.999
4.500
0.835
0.02018
-0.0607
0.500
1.000
-99.999
-99.999
5.000
0.897
0.02220
-0.0621
0.477
1.000
-99.999
-99.999
5.500
0.904
0.02235
-0.0522
0.426
1.000
-99.999
-99.999
6.000
0.888
0.02245
-0.0384
0.373
1.000
-99.999
-99.999
6.500
0.876
0.02313
-0.0254
0.318
1.000
-99.999
-99.999
7.000
0.865
0.02430
-0.0131
0.254
1.000
-99.999
-99.999
7.500
0.865
0.02663
-0.0043
0.181
1.000
-99.999
-99.999
8.000
0.870
0.02960
0.0029
0.122
1.000
-99.999
-99.999
8.500
0.886
0.03331
0.0081
0.080
1.000
-99.999
-99.999
9.000
0.909
0.03747
0.0120
0.052
1.000
-99.999
-99.999
9.500
0.941
0.04309
0.0143
0.037
1.000
-99.999
-99.999
10.000
0.952
0.04859
0.0182
0.029
1.000
-99.999
-99.999
10.500
0.943
0.05484
0.0227
0.025
1.000
-99.999
-99.999
11.000
0.920
0.06182
0.0249
0.023
1.000
-99.999
-99.999
11.500
0.881
0.07131
0.0224
0.023
1.000
-99.999
-99.999
12.000
0.825
0.08578
0.0120
0.026
1.000
-99.999
-99.999
12.500
0.759
0.11280
-0.0093
0.031
1.000
-99.999
-99.999
polar
100000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.098
0.01249
-0.0176
0.500
0.864
-99.999
-99.999
-1.500
0.041
0.01239
-0.0321
0.500
1.000
-99.999
-99.999
-1.000
0.086
0.01224
-0.0311
0.500
1.000
-99.999
-99.999
-0.500
0.134
0.01221
-0.0303
0.500
1.000
-99.999
-99.999
0.000
0.184
0.01224
-0.0295
0.500
1.000
-99.999
-99.999
0.500
0.235
0.01231
-0.0289
0.500
1.000
-99.999
-99.999
1.000
0.287
0.01241
-0.0283
0.500
1.000
-99.999
-99.999
1.500
0.341
0.01255
-0.0279
0.500
1.000
-99.999
-99.999
2.000
0.394
0.01273
-0.0276
0.500
1.000
-99.999
-99.999
2.500
0.448
0.01294
-0.0274
0.500
1.000
-99.999
-99.999
3.000
0.503
0.01319
-0.0272
0.500
1.000
-99.999
-99.999
3.500
0.558
0.01351
-0.0271
0.500
1.000
-99.999
-99.999
4.000
0.613
0.01390
-0.0271
0.500
1.000
-99.999
-99.999
4.500
0.669
0.01445
-0.0273
0.500
1.000
-99.999
-99.999
5.000
0.726
0.01537
-0.0279
0.500
1.000
-99.999
-99.999
5.500
0.775
0.01589
-0.0261
0.444
1.000
-99.999
-99.999
6.000
0.820
0.01669
-0.0239
0.362
1.000
-99.999
-99.999
6.500
0.861
0.01826
-0.0221
0.256
1.000
-99.999
-99.999
7.000
0.900
0.02063
-0.0206
0.143
1.000
-99.999
-99.999
7.500
0.935
0.02384
-0.0184
0.072
1.000
-99.999
-99.999
8.000
0.967
0.02754
-0.0157
0.040
1.000
-99.999
-99.999
8.500
1.002
0.03174
-0.0130
0.026
1.000
-99.999
-99.999
9.000
1.036
0.03717
-0.0105
0.018
1.000
-99.999
-99.999
9.500
1.064
0.04208
-0.0086
0.014
1.000
-99.999
-99.999
10.000
1.077
0.05007
-0.0063
0.011
1.000
-99.999
-99.999
10.500
1.076
0.05788
-0.0047
0.009
1.000
-99.999
-99.999
11.000
1.052
0.06649
-0.0045
0.009
1.000
-99.999
-99.999
11.500
1.014
0.07796
-0.0100
0.009
1.000
-99.999
-99.999
12.000
0.960
0.09576
-0.0242
0.010
1.000
-99.999
-99.999
polar
200000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.076
0.01028
-0.0247
0.500
0.629
-99.999
-99.999
-1.500
-0.034
0.00946
-0.0205
0.500
0.841
-99.999
-99.999
-1.000
0.036
0.00933
-0.0216
0.500
0.960
-99.999
-99.999
-0.500
0.141
0.00929
-0.0317
0.500
1.000
-99.999
-99.999
0.000
0.190
0.00929
-0.0308
0.500
1.000
-99.999
-99.999
0.500
0.240
0.00933
-0.0300
0.500
1.000
-99.999
-99.999
1.000
0.292
0.00941
-0.0292
0.500
1.000
-99.999
-99.999
1.500
0.344
0.00951
-0.0286
0.500
1.000
-99.999
-99.999
2.000
0.397
0.00963
-0.0281
0.500
1.000
-99.999
-99.999
2.500
0.451
0.00979
-0.0278
0.500
1.000
-99.999
-99.999
3.000
0.506
0.00997
-0.0276
0.500
1.000
-99.999
-99.999
3.500
0.561
0.01019
-0.0274
0.500
1.000
-99.999
-99.999
4.000
0.616
0.01048
-0.0273
0.500
1.000
-99.999
-99.999
4.500
0.670
0.01087
-0.0270
0.482
1.000
-99.999
-99.999
5.000
0.721
0.01142
-0.0261
0.423
1.000
-99.999
-99.999
5.500
0.770
0.01222
-0.0252
0.348
1.000
-99.999
-99.999
6.000
0.817
0.01338
-0.0244
0.256
1.000
-99.999
-99.999
6.500
0.863
0.01494
-0.0236
0.156
1.000
-99.999
-99.999
7.000
0.907
0.01683
-0.0225
0.076
1.000
-99.999
-99.999
7.500
0.949
0.01914
-0.0209
0.036
1.000
-99.999
-99.999
8.000
0.982
0.02244
-0.0183
0.019
1.000
-99.999
-99.999
8.500
1.015
0.02572
-0.0158
0.012
1.000
-99.999
-99.999
9.000
1.048
0.02913
-0.0135
0.007
1.000
-99.999
-99.999
9.500
1.075
0.03412
-0.0108
0.005
1.000
-99.999
-99.999
10.000
1.096
0.03942
-0.0084
0.004
1.000
-99.999
-99.999
10.500
1.100
0.04698
-0.0053
0.003
1.000
-99.999
-99.999
11.000
1.085
0.05545
-0.0036
0.003
1.000
-99.999
-99.999
11.500
1.057
0.06520
-0.0059
0.003
1.000
-99.999
-99.999
12.000
1.023
0.07718
-0.0131
0.003
1.000
-99.999
-99.999
12.500
0.983
0.09287
-0.0259
0.003
1.000
-99.999
-99.999
polar
400000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.069
0.00918
-0.0255
0.500
0.413
-99.999
-99.999
-1.500
-0.018
0.00836
-0.0248
0.500
0.602
-99.999
-99.999
-1.000
0.031
0.00761
-0.0229
0.500
0.791
-99.999
-99.999
-0.500
0.078
0.00723
-0.0200
0.500
0.915
-99.999
-99.999
0.000
0.154
0.00721
-0.0237
0.500
0.984
-99.999
-99.999
0.500
0.244
0.00723
-0.0310
0.500
1.000
-99.999
-99.999
1.000
0.294
0.00728
-0.0301
0.500
1.000
-99.999
-99.999
1.500
0.346
0.00734
-0.0293
0.500
1.000
-99.999
-99.999
2.000
0.399
0.00743
-0.0287
0.500
1.000
-99.999
-99.999
2.500
0.452
0.00753
-0.0282
0.500
1.000
-99.999
-99.999
3.000
0.507
0.00765
-0.0279
0.500
1.000
-99.999
-99.999
3.500
0.562
0.00781
-0.0277
0.500
1.000
-99.999
-99.999
4.000
0.614
0.00819
-0.0272
0.456
1.000
-99.999
-99.999
4.500
0.666
0.00870
-0.0267
0.402
1.000
-99.999
-99.999
5.000
0.718
0.00941
-0.0262
0.334
1.000
-99.999
-99.999
5.500
0.768
0.01032
-0.0258
0.256
1.000
-99.999
-99.999
6.000
0.817
0.01146
-0.0254
0.171
1.000
-99.999
-99.999
6.500
0.865
0.01279
-0.0248
0.093
1.000
-99.999
-99.999
7.000
0.912
0.01421
-0.0241
0.039
1.000
-99.999
-99.999
7.500
0.957
0.01596
-0.0228
0.018
1.000
-99.999
-99.999
8.000
0.999
0.01805
-0.0212
0.008
1.000
-99.999
-99.999
10.500
1.027
0.03209
0.0127
0.002
1.000
-99.999
-99.999
11.000
1.032
0.03714
0.0154
0.002
1.000
-99.999
-99.999
11.500
1.027
0.04360
0.0168
0.001
1.000
-99.999
-99.999
12.000
1.015
0.05102
0.0159
0.001
1.000
-99.999
-99.999
12.500
0.991
0.06074
0.0118
0.001
1.000
-99.999
-99.999
13.000
0.957
0.07363
0.0034
0.001
1.000
-99.999
-99.999
13.500
0.928
0.08803
-0.0081
0.001
1.000
-99.999
-99.999
polar
600000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-2.000
-0.068
0.00868
-0.0253
0.500
0.289
-99.999
-99.999
-1.500
-0.014
0.00784
-0.0251
0.500
0.484
-99.999
-99.999
-1.000
0.038
0.00718
-0.0246
0.500
0.654
-99.999
-99.999
-0.500
0.090
0.00665
-0.0234
0.500
0.798
-99.999
-99.999
0.000
0.139
0.00629
-0.0212
0.500
0.910
-99.999
-99.999
0.500
0.205
0.00623
-0.0228
0.500
0.984
-99.999
-99.999
1.000
0.295
0.00627
-0.0304
0.500
1.000
-99.999
-99.999
1.500
0.349
0.00632
-0.0300
0.500
1.000
-99.999
-99.999
2.000
0.401
0.00639
-0.0292
0.500
1.000
-99.999
-99.999
2.500
0.454
0.00648
-0.0286
0.500
1.000
-99.999
-99.999
3.000
0.508
0.00660
-0.0282
0.496
1.000
-99.999
-99.999
3.500
0.560
0.00693
-0.0277
0.456
1.000
-99.999
-99.999
4.000
0.613
0.00736
-0.0272
0.406
1.000
-99.999
-99.999
4.500
0.665
0.00792
-0.0269
0.347
1.000
-99.999
-99.999
5.000
0.718
0.00856
-0.0266
0.288
1.000
-99.999
-99.999
5.500
0.768
0.00955
-0.0262
0.202
1.000
-99.999
-99.999
6.000
0.817
0.01076
-0.0258
0.116
1.000
-99.999
-99.999
6.500
0.867
0.01188
-0.0253
0.059
1.000
-99.999
-99.999
7.000
0.916
0.01298
-0.0248
0.027
1.000
-99.999
-99.999
7.500
0.962
0.01457
-0.0236
0.011
1.000
-99.999
-99.999
8.000
1.005
0.01655
-0.0222
0.003
1.000
-99.999
-99.999
8.500
1.047
0.01851
-0.0207
0.002
1.000
-99.999
-99.999
9.000
1.081
0.02130
-0.0184
0.001
1.000
-99.999
-99.999
9.500
1.107
0.02518
-0.0152
0.001
1.000
-99.999
-99.999
10.000
1.127
0.03027
-0.0118
0.001
1.000
-99.999
-99.999
10.500
1.136
0.03640
-0.0079
0.001
1.000
-99.999
-99.999
11.000
1.130
0.04348
-0.0049
0.001
1.000
-99.999
-99.999
11.500
1.112
0.05184
-0.0047
0.001
1.000
-99.999
-99.999
12.000
1.085
0.06190
-0.0083
0.001
1.000
-99.999
-99.999
12.500
1.051
0.07452
-0.0166
0.001
1.000
-99.999
-99.999
13.000
1.014
0.09080
-0.0296
0.001
1.000
-99.999
-99.999