S809 UNVENTED AILERON, CLEAN, CHORD = 18 INCHES
          
---------
         
Run Conditions: vel=210.2 ft/s  Re=1.992x10^6  AOA=-5.97  Flap deflection=-90.00
Totals: Cl=-1.4934  Cdp=0.6072  Cm(c/4)=0.1674  Cs=-0.4486  Ch=0.5234
Main component: Cl=-1.4919  Cdp=0.0800  Cm=0.4032
Flap component: Cl=-0.0014  Cdp=0.5271  Cm=0.1513
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.9329
0.6175, -0.04610, -0.8946
0.5841, -0.02440, -0.8926
0.5775, 0.01750, -0.8942
0.5777, 0.04660, -0.8851
0.6274, 0.07170, 0.9351
0.5694, 0.08320, 0.9282
0.5112, 0.09370, 0.9304
0.4731, 0.09830, 0.9280
0.4349, 0.10070, 0.8947
0.3960, 0.10120, 0.8430
0.3566, 0.10020, 0.8182
0.3172, 0.09790, 0.8050
0.2778, 0.09440, 0.7966
0.2393, 0.08960, 0.8020
0.2056, 0.08360, 0.8205
0.1633, 0.07610, 0.8537
0.1261, 0.06710, 0.9031
0.0900, 0.05640, 0.9627
0.0571, 0.04390, 1.0092
0.0283, 0.02940, 0.9429
0.0142, 0.01970, 0.6424
0.0081, 0.01410, 0.2334
0.0026, 0.00780, -0.7317
0.0000, 0.00000, -3.0244
0.0037, -0.00840, -2.5791
0.0112, -0.01420, -2.5667
0.0191, -0.01930, -2.5802
0.0397, -0.03030, -2.6265
0.0706, -0.04420, -2.6699
0.1037, -0.05710, -2.5459
0.1384, -0.06890, -2.2957
0.1741, -0.07950, -2.0322
0.2102, -0.08660, -1.8118
0.2472, -0.09640, -1.5942
0.2844, -0.10270, -1.4392
0.3225, -0.10690, -1.3321
0.3608, -0.10890, -1.2460
0.3991, -0.10830, -1.1518
0.4373, -0.10510, -1.0879
0.4757, -0.09890, -1.0428
0.5137, -0.09070, -0.9981
0.5694, -0.07640, -0.9562
         
15 Flap element taps
1.0000, 0.00130, -0.8312
0.9365, 0.01390, 0.6375
0.8333, 0.03280, 0.9209
0.7436, 0.04930, 0.9316
0.7049, 0.05670, 0.9289
0.6662, 0.06410, 0.9351
0.6522, 0.01390, -0.8996
0.5969, -0.00020, -0.9185
0.6000, -0.03020, -0.9083
0.6324, -0.04540, -0.9095
0.6667, -0.04880, -0.8923
0.7046, -0.04110, -0.8574
0.7429, -0.03210, -0.8508
0.8333, -0.01400, -0.8431
0.9311, -0.00120, -0.8309
            
---------
         
Run Conditions: vel=214.9 ft/s  Re=2.033x10^6  AOA=-0.01  Flap deflection=-90.00
Totals: Cl=-1.6786  Cdp=0.4140  Cm(c/4)=0.1921  Cs=-0.4137  Ch=0.5068
Main component: Cl=-1.6287  Cdp=-0.0935  Cm=0.4682
Flap component: Cl=-0.0499  Cdp=0.5075  Cm=0.1436
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.8701
0.6175, -0.04610, -0.8126
0.5841, -0.02440, -0.8107
0.5775, 0.01750, -0.8161
0.5777, 0.04660, -0.8102
0.6274, 0.07170, 0.9172
0.5694, 0.08320, 0.9068
0.5112, 0.09370, 0.9146
0.4731, 0.09830, 0.9125
0.4349, 0.10070, 0.8821
0.3960, 0.10120, 0.8336
0.3566, 0.10020, 0.7772
0.3172, 0.09790, 0.7622
0.2778, 0.09440, 0.7467
0.2393, 0.08960, 0.7434
0.2056, 0.08360, 0.7547
0.1633, 0.07610, 0.7858
0.1261, 0.06710, 0.8374
0.0900, 0.05640, 0.9090
0.0571, 0.04390, 0.9885
0.0283, 0.02940, 0.9911
0.0142, 0.01970, 0.7565
0.0081, 0.01410, 0.3594
0.0026, 0.00780, -0.7677
0.0000, 0.00000, -4.8930
0.0037, -0.00840, -5.5340
0.0112, -0.01420, -3.5114
0.0191, -0.01930, -2.8245
0.0397, -0.03030, -2.1436
0.0706, -0.04420, -1.8728
0.1037, -0.05710, -1.8303
0.1384, -0.06890, -1.8330
0.1741, -0.07950, -1.8445
0.2102, -0.08660, -1.9185
0.2472, -0.09640, -2.0353
0.2844, -0.10270, -2.0746
0.3225, -0.10690, -2.1092
0.3608, -0.10890, -2.1237
0.3991, -0.10830, -2.0456
0.4373, -0.10510, -1.8803
0.4757, -0.09890, -1.5994
0.5137, -0.09070, -1.3260
0.5694, -0.07640, -1.0038
         
15 Flap element taps
1.0000, 0.00130, -0.8117
0.9365, 0.01390, 0.6203
0.8333, 0.03280, 0.9128
0.7436, 0.04930, 0.9144
0.7049, 0.05670, 0.9085
0.6662, 0.06410, 0.9189
0.6522, 0.01390, -0.8137
0.5969, -0.00020, -0.8196
0.6000, -0.03020, -0.8163
0.6324, -0.04540, -0.8160
0.6667, -0.04880, -0.8161
0.7046, -0.04110, -0.8061
0.7429, -0.03210, -0.8082
0.8333, -0.01400, -0.8095
0.9311, -0.00120, -0.8042
            
---------
         
Run Conditions: vel=211.5 ft/s  Re=2.002x10^6  AOA=2.99  Flap deflection=-90.00
Totals: Cl=-1.7270  Cdp=0.4446  Cm(c/4)=0.2260  Cs=-0.5341  Ch=0.5597
Main component: Cl=-1.6444  Cdp=-0.1124  Cm=0.4940
Flap component: Cl=-0.0825  Cdp=0.5570  Cm=0.1574
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.0882
0.6175, -0.04610, -0.9746
0.5841, -0.02440, -0.9766
0.5775, 0.01750, -0.9911
0.5777, 0.04660, -0.9823
0.6274, 0.07170, 0.9001
0.5694, 0.08320, 0.8906
0.5112, 0.09370, 0.8955
0.4731, 0.09830, 0.8929
0.4349, 0.10070, 0.8635
0.3960, 0.10120, 0.8083
0.3566, 0.10020, 0.7443
0.3172, 0.09790, 0.7237
0.2778, 0.09440, 0.7051
0.2393, 0.08960, 0.6968
0.2056, 0.08360, 0.7035
0.1633, 0.07610, 0.7313
0.1261, 0.06710, 0.7813
0.0900, 0.05640, 0.8557
0.0571, 0.04390, 0.9510
0.0283, 0.02940, 1.0040
0.0142, 0.01970, 0.8652
0.0081, 0.01410, 0.5730
0.0026, 0.00780, -0.3600
0.0000, 0.00000, -3.7652
0.0037, -0.00840, -4.5519
0.0112, -0.01420, -3.0642
0.0191, -0.01930, -2.3871
0.0397, -0.03030, -1.8776
0.0706, -0.04420, -1.6923
0.1037, -0.05710, -1.7002
0.1384, -0.06890, -1.7426
0.1741, -0.07950, -1.7889
0.2102, -0.08660, -1.8967
0.2472, -0.09640, -2.0485
0.2844, -0.10270, -2.1251
0.3225, -0.10690, -2.1997
0.3608, -0.10890, -2.2610
0.3991, -0.10830, -2.2317
0.4373, -0.10510, -2.1221
0.4757, -0.09890, -1.8927
0.5137, -0.09070, -1.6631
0.5694, -0.07640, -1.3009
         
15 Flap element taps
1.0000, 0.00130, -0.9962
0.9365, 0.01390, 0.5852
0.8333, 0.03280, 0.8966
0.7436, 0.04930, 0.8914
0.7049, 0.05670, 0.8869
0.6662, 0.06410, 0.8970
0.6522, 0.01390, -0.9783
0.5969, -0.00020, -0.9906
0.6000, -0.03020, -0.9881
0.6324, -0.04540, -0.9991
0.6667, -0.04880, -1.0096
0.7046, -0.04110, -0.9981
0.7429, -0.03210, -0.9949
0.8333, -0.01400, -1.0011
0.9311, -0.00120, -1.0030
            
---------
         
Run Conditions: vel=211.6 ft/s  Re=1.997x10^6  AOA=6.01  Flap deflection=-90.00
Totals: Cl=-1.5977  Cdp=0.4696  Cm(c/4)=0.2424  Cs=-0.6343  Ch=0.5779
Main component: Cl=-1.4828  Cdp=-0.1021  Cm=0.4652
Flap component: Cl=-0.1149  Cdp=0.5716  Cm=0.1622
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.1348
0.6175, -0.04610, -1.0419
0.5841, -0.02440, -1.0385
0.5775, 0.01750, -1.0438
0.5777, 0.04660, -1.0353
0.6274, 0.07170, 0.8758
0.5694, 0.08320, 0.8603
0.5112, 0.09370, 0.8714
0.4731, 0.09830, 0.8735
0.4349, 0.10070, 0.8502
0.3960, 0.10120, 0.7865
0.3566, 0.10020, 0.7345
0.3172, 0.09790, 0.6670
0.2778, 0.09440, 0.6463
0.2393, 0.08960, 0.6263
0.2056, 0.08360, 0.6204
0.1633, 0.07610, 0.6363
0.1261, 0.06710, 0.6774
0.0900, 0.05640, 0.7462
0.0571, 0.04390, 0.8570
0.0283, 0.02940, 0.9866
0.0142, 0.01970, 0.9966
0.0081, 0.01410, 0.8834
0.0026, 0.00780, 0.2730
0.0000, 0.00000, -1.7654
0.0037, -0.00840, -2.7052
0.0112, -0.01420, -2.2173
0.0191, -0.01930, -1.5555
0.0397, -0.03030, -1.2844
0.0706, -0.04420, -1.2421
0.1037, -0.05710, -1.3212
0.1384, -0.06890, -1.4140
0.1741, -0.07950, -1.4980
0.2102, -0.08660, -1.6383
0.2472, -0.09640, -1.8161
0.2844, -0.10270, -1.9220
0.3225, -0.10690, -2.0277
0.3608, -0.10890, -2.1203
0.3991, -0.10830, -2.1272
0.4373, -0.10510, -2.0559
0.4757, -0.09890, -1.8638
0.5137, -0.09070, -1.6676
0.5694, -0.07640, -1.3336
         
15 Flap element taps
1.0000, 0.00130, -1.0446
0.9365, 0.01390, 0.5627
0.8333, 0.03280, 0.8916
0.7436, 0.04930, 0.8684
0.7049, 0.05670, 0.8631
0.6662, 0.06410, 0.8786
0.6522, 0.01390, -1.0443
0.5969, -0.00020, -1.0584
0.6000, -0.03020, -1.0562
0.6324, -0.04540, -1.0749
0.6667, -0.04880, -1.0982
0.7046, -0.04110, -1.0869
0.7429, -0.03210, -1.0883
0.8333, -0.01400, -1.0824
0.9311, -0.00120, -1.0650
            
---------
         
Run Conditions: vel=211.2 ft/s  Re=1.994x10^6  AOA=9.01  Flap deflection=-90.00
Totals: Cl=-1.4776  Cdp=0.4732  Cm(c/4)=0.2547  Cs=-0.6987  Ch=0.5853
Main component: Cl=-1.3313  Cdp=-0.0964  Cm=0.4368
Flap component: Cl=-0.1463  Cdp=0.5696  Cm=0.1642
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.1457
0.6175, -0.04610, -1.0907
0.5841, -0.02440, -1.0815
0.5775, 0.01750, -1.0927
0.5777, 0.04660, -1.0832
0.6274, 0.07170, 0.8537
0.5694, 0.08320, 0.8317
0.5112, 0.09370, 0.8478
0.4731, 0.09830, 0.8492
0.4349, 0.10070, 0.8341
0.3960, 0.10120, 0.7684
0.3566, 0.10020, 0.6990
0.3172, 0.09790, 0.6304
0.2778, 0.09440, 0.5792
0.2393, 0.08960, 0.5515
0.2056, 0.08360, 0.5313
0.1633, 0.07610, 0.5300
0.1261, 0.06710, 0.5567
0.0900, 0.05640, 0.6109
0.0571, 0.04390, 0.7173
0.0283, 0.02940, 0.8828
0.0142, 0.01970, 0.9979
0.0081, 0.01410, 1.0043
0.0026, 0.00780, 0.7640
0.0000, 0.00000, -0.3233
0.0037, -0.00840, -1.2891
0.0112, -0.01420, -1.1075
0.0191, -0.01930, -0.9624
0.0397, -0.03030, -0.8187
0.0706, -0.04420, -0.8562
0.1037, -0.05710, -0.9850
0.1384, -0.06890, -1.1163
0.1741, -0.07950, -1.2522
0.2102, -0.08660, -1.4118
0.2472, -0.09640, -1.6080
0.2844, -0.10270, -1.7414
0.3225, -0.10690, -1.8887
0.3608, -0.10890, -2.0052
0.3991, -0.10830, -2.0567
0.4373, -0.10510, -1.9969
0.4757, -0.09890, -1.8597
0.5137, -0.09070, -1.6657
0.5694, -0.07640, -1.2909
         
15 Flap element taps
1.0000, 0.00130, -1.0857
0.9365, 0.01390, 0.5439
0.8333, 0.03280, 0.8796
0.7436, 0.04930, 0.8353
0.7049, 0.05670, 0.8344
0.6662, 0.06410, 0.8520
0.6522, 0.01390, -1.0868
0.5969, -0.00020, -1.1019
0.6000, -0.03020, -1.0946
0.6324, -0.04540, -1.1088
0.6667, -0.04880, -1.1308
0.7046, -0.04110, -1.1116
0.7429, -0.03210, -1.1169
0.8333, -0.01400, -1.1351
0.9311, -0.00120, -1.1053
            
---------
         
Run Conditions: vel=211.4 ft/s  Re=1.988x10^6  AOA=12.06  Flap deflection=-90.00
Totals: Cl=-1.3041  Cdp=0.4773  Cm(c/4)=0.2613  Cs=-0.7393  Ch=0.5822
Main component: Cl=-1.1284  Cdp=-0.0794  Cm=0.3916
Flap component: Cl=-0.1757  Cdp=0.5568  Cm=0.1636
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.1301
0.6175, -0.04610, -1.1049
0.5841, -0.02440, -1.1071
0.5775, 0.01750, -1.1142
0.5777, 0.04660, -1.1042
0.6274, 0.07170, 0.8141
0.5694, 0.08320, 0.7905
0.5112, 0.09370, 0.8045
0.4731, 0.09830, 0.8109
0.4349, 0.10070, 0.8049
0.3960, 0.10120, 0.7480
0.3566, 0.10020, 0.6602
0.3172, 0.09790, 0.5996
0.2778, 0.09440, 0.4890
0.2393, 0.08960, 0.4605
0.2056, 0.08360, 0.4268
0.1633, 0.07610, 0.4047
0.1261, 0.06710, 0.4096
0.0900, 0.05640, 0.4372
0.0571, 0.04390, 0.5182
0.0283, 0.02940, 0.6765
0.0142, 0.01970, 0.8511
0.0081, 0.01410, 0.9455
0.0026, 0.00780, 0.9705
0.0000, 0.00000, 0.6397
0.0037, -0.00840, -0.1389
0.0112, -0.01420, -0.2459
0.0191, -0.01930, -0.2611
0.0397, -0.03030, -0.3086
0.0706, -0.04420, -0.4435
0.1037, -0.05710, -0.6153
0.1384, -0.06890, -0.7797
0.1741, -0.07950, -0.9400
0.2102, -0.08660, -1.1176
0.2472, -0.09640, -1.3294
0.2844, -0.10270, -1.4815
0.3225, -0.10690, -1.6496
0.3608, -0.10890, -1.7865
0.3991, -0.10830, -1.8676
0.4373, -0.10510, -1.8391
0.4757, -0.09890, -1.7276
0.5137, -0.09070, -1.5733
0.5694, -0.07640, -1.2359
         
15 Flap element taps
1.0000, 0.00130, -1.1133
0.9365, 0.01390, 0.5212
0.8333, 0.03280, 0.8624
0.7436, 0.04930, 0.7946
0.7049, 0.05670, 0.7933
0.6662, 0.06410, 0.8166
0.6522, 0.01390, -1.1107
0.5969, -0.00020, -1.1201
0.6000, -0.03020, -1.1149
0.6324, -0.04540, -1.1276
0.6667, -0.04880, -1.1490
0.7046, -0.04110, -1.1361
0.7429, -0.03210, -1.1312
0.8333, -0.01400, -1.1423
0.9311, -0.00120, -1.1231
            
---------
         
Run Conditions: vel=212.8 ft/s  Re=1.995x10^6  AOA=14.99  Flap deflection=-90.00
Totals: Cl=-1.1303  Cdp=0.4770  Cm(c/4)=0.2651  Cs=-0.7531  Ch=0.5731
Main component: Cl=-0.9290  Cdp=-0.0583  Cm=0.3455
Flap component: Cl=-0.2013  Cdp=0.5353  Cm=0.1618
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.1154
0.6175, -0.04610, -1.1514
0.5841, -0.02440, -1.1397
0.5775, 0.01750, -1.1243
0.5777, 0.04660, -1.1204
0.6274, 0.07170, 0.7744
0.5694, 0.08320, 0.7234
0.5112, 0.09370, 0.7540
0.4731, 0.09830, 0.7688
0.4349, 0.10070, 0.7702
0.3960, 0.10120, 0.7433
0.3566, 0.10020, 0.6502
0.3172, 0.09790, 0.5603
0.2778, 0.09440, 0.4861
0.2393, 0.08960, 0.3587
0.2056, 0.08360, 0.3187
0.1633, 0.07610, 0.2736
0.1261, 0.06710, 0.2487
0.0900, 0.05640, 0.2377
0.0571, 0.04390, 0.2717
0.0283, 0.02940, 0.3768
0.0142, 0.01970, 0.5438
0.0081, 0.01410, 0.6751
0.0026, 0.00780, 0.8380
0.0000, 0.00000, 1.0034
0.0037, -0.00840, 0.6198
0.0112, -0.01420, 0.3910
0.0191, -0.01930, 0.2858
0.0397, -0.03030, 0.1215
0.0706, -0.04420, -0.0766
0.1037, -0.05710, -0.2778
0.1384, -0.06890, -0.4651
0.1741, -0.07950, -0.6449
0.2102, -0.08660, -0.8331
0.2472, -0.09640, -1.0545
0.2844, -0.10270, -1.2222
0.3225, -0.10690, -1.4044
0.3608, -0.10890, -1.5562
0.3991, -0.10830, -1.6623
0.4373, -0.10510, -1.6600
0.4757, -0.09890, -1.5757
0.5137, -0.09070, -1.4703
0.5694, -0.07640, -1.1957
         
15 Flap element taps
1.0000, 0.00130, -1.1010
0.9365, 0.01390, 0.5160
0.8333, 0.03280, 0.8427
0.7436, 0.04930, 0.7368
0.7049, 0.05670, 0.7397
0.6662, 0.06410, 0.7754
0.6522, 0.01390, -1.1176
0.5969, -0.00020, -1.1314
0.6000, -0.03020, -1.1256
0.6324, -0.04540, -1.1279
0.6667, -0.04880, -1.1411
0.7046, -0.04110, -1.1274
0.7429, -0.03210, -1.1328
0.8333, -0.01400, -1.1360
0.9311, -0.00120, -1.1068
            
---------
         
Run Conditions: vel=213.4 ft/s  Re=1.998x10^6  AOA=17.99  Flap deflection=-90.00
Totals: Cl=-0.9350  Cdp=0.4699  Cm(c/4)=0.2631  Cs=-0.7357  Ch=0.5584
Main component: Cl=-0.7157  Cdp=-0.0351  Cm=0.2932
Flap component: Cl=-0.2193  Cdp=0.5050  Cm=0.1559
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.0826
0.6175, -0.04610, -1.1194
0.5841, -0.02440, -1.1414
0.5775, 0.01750, -1.1428
0.5777, 0.04660, -1.1381
0.6274, 0.07170, 0.7033
0.5694, 0.08320, 0.6432
0.5112, 0.09370, 0.6680
0.4731, 0.09830, 0.6722
0.4349, 0.10070, 0.6775
0.3960, 0.10120, 0.6772
0.3566, 0.10020, 0.6340
0.3172, 0.09790, 0.5314
0.2778, 0.09440, 0.4145
0.2393, 0.08960, 0.3146
0.2056, 0.08360, 0.2078
0.1633, 0.07610, 0.1161
0.1261, 0.06710, 0.0629
0.0900, 0.05640, 0.0059
0.0571, 0.04390, -0.0306
0.0283, 0.02940, -0.0193
0.0142, 0.01970, 0.0700
0.0081, 0.01410, 0.1667
0.0026, 0.00780, 0.3398
0.0000, 0.00000, 0.8183
0.0037, -0.00840, 0.9726
0.0112, -0.01420, 0.8019
0.0191, -0.01930, 0.6797
0.0397, -0.03030, 0.4705
0.0706, -0.04420, 0.2446
0.1037, -0.05710, 0.0314
0.1384, -0.06890, -0.1681
0.1741, -0.07950, -0.3568
0.2102, -0.08660, -0.5513
0.2472, -0.09640, -0.7776
0.2844, -0.10270, -0.9565
0.3225, -0.10690, -1.1509
0.3608, -0.10890, -1.3180
0.3991, -0.10830, -1.4441
0.4373, -0.10510, -1.4694
0.4757, -0.09890, -1.4110
0.5137, -0.09070, -1.3497
0.5694, -0.07640, -1.1069
         
15 Flap element taps
1.0000, 0.00130, -1.1348
0.9365, 0.01390, 0.5041
0.8333, 0.03280, 0.7672
0.7436, 0.04930, 0.6318
0.7049, 0.05670, 0.6421
0.6662, 0.06410, 0.6871
0.6522, 0.01390, -1.0965
0.5969, -0.00020, -1.1160
0.6000, -0.03020, -1.1030
0.6324, -0.04540, -1.1058
0.6667, -0.04880, -1.1229
0.7046, -0.04110, -1.1170
0.7429, -0.03210, -1.1191
0.8333, -0.01400, -1.1304
0.9311, -0.00120, -1.1353
            
---------
         
Run Conditions: vel=213.4 ft/s  Re=1.999x10^6  AOA=19.95  Flap deflection=-90.00
Totals: Cl=-0.7988  Cdp=0.4634  Cm(c/4)=0.2571  Cs=-0.7081  Ch=0.5435
Main component: Cl=-0.5697  Cdp=-0.0146  Cm=0.2531
Flap component: Cl=-0.2291  Cdp=0.4779  Cm=0.1522
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -1.0382
0.6175, -0.04610, -1.1065
0.5841, -0.02440, -1.1187
0.5775, 0.01750, -1.1296
0.5777, 0.04660, -1.1242
0.6274, 0.07170, 0.6093
0.5694, 0.08320, 0.5230
0.5112, 0.09370, 0.5485
0.4731, 0.09830, 0.5699
0.4349, 0.10070, 0.5752
0.3960, 0.10120, 0.5793
0.3566, 0.10020, 0.5701
0.3172, 0.09790, 0.5389
0.2778, 0.09440, 0.4355
0.2393, 0.08960, 0.3012
0.2056, 0.08360, 0.1785
0.1633, 0.07610, 0.0725
0.1261, 0.06710, -0.0513
0.0900, 0.05640, -0.1497
0.0571, 0.04390, -0.2449
0.0283, 0.02940, -0.3240
0.0142, 0.01970, -0.3292
0.0081, 0.01410, -0.3041
0.0026, 0.00780, -0.1202
0.0000, 0.00000, 0.3341
0.0037, -0.00840, 1.0056
0.0112, -0.01420, 0.9567
0.0191, -0.01930, 0.8605
0.0397, -0.03030, 0.6596
0.0706, -0.04420, 0.4326
0.1037, -0.05710, 0.2192
0.1384, -0.06890, 0.0159
0.1741, -0.07950, -0.1746
0.2102, -0.08660, -0.3698
0.2472, -0.09640, -0.5973
0.2844, -0.10270, -0.7809
0.3225, -0.10690, -0.9812
0.3608, -0.10890, -1.1559
0.3991, -0.10830, -1.2948
0.4373, -0.10510, -1.3369
0.4757, -0.09890, -1.2955
0.5137, -0.09070, -1.2624
0.5694, -0.07640, -1.0414
         
15 Flap element taps
1.0000, 0.00130, -1.1185
0.9365, 0.01390, 0.5211
0.8333, 0.03280, 0.7051
0.7436, 0.04930, 0.5355
0.7049, 0.05670, 0.5504
0.6662, 0.06410, 0.6089
0.6522, 0.01390, -1.0968
0.5969, -0.00020, -1.1178
0.6000, -0.03020, -1.1027
0.6324, -0.04540, -1.1011
0.6667, -0.04880, -1.1164
0.7046, -0.04110, -1.1084
0.7429, -0.03210, -1.1102
0.8333, -0.01400, -1.1136
0.9311, -0.00120, -1.1202
            
---------
         
Run Conditions: vel=214.3 ft/s  Re=2.004x10^6  AOA=23.99  Flap deflection=-90.00
Totals: Cl=-0.4118  Cdp=0.4283  Cm(c/4)=0.2125  Cs=-0.5588  Ch=0.4459
Main component: Cl=-0.2023  Cdp=0.0589  Cm=0.1399
Flap component: Cl=-0.2095  Cdp=0.3695  Cm=0.1231
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.9232
0.6175, -0.04610, -1.0752
0.5841, -0.02440, -1.0674
0.5775, 0.01750, -1.0681
0.5777, 0.04660, -1.0637
0.6274, 0.07170, 0.3129
0.5694, 0.08320, 0.1644
0.5112, 0.09370, 0.1547
0.4731, 0.09830, 0.1689
0.4349, 0.10070, 0.1969
0.3960, 0.10120, 0.2124
0.3566, 0.10020, 0.2093
0.3172, 0.09790, 0.2190
0.2778, 0.09440, 0.2238
0.2393, 0.08960, 0.2220
0.2056, 0.08360, 0.1803
0.1633, 0.07610, 0.0163
0.1261, 0.06710, -0.2032
0.0900, 0.05640, -0.4467
0.0571, 0.04390, -0.7201
0.0283, 0.02940, -1.0691
0.0142, 0.01970, -1.4332
0.0081, 0.01410, -1.7043
0.0026, 0.00780, -1.7407
0.0000, 0.00000, -1.7994
0.0037, -0.00840, 0.5633
0.0112, -0.01420, 0.9695
0.0191, -0.01930, 1.0118
0.0397, -0.03030, 0.9325
0.0706, -0.04420, 0.7552
0.1037, -0.05710, 0.5681
0.1384, -0.06890, 0.3753
0.1741, -0.07950, 0.1926
0.2102, -0.08660, 0.0043
0.2472, -0.09640, -0.2151
0.2844, -0.10270, -0.4020
0.3225, -0.10690, -0.6063
0.3608, -0.10890, -0.7913
0.3991, -0.10830, -0.9491
0.4373, -0.10510, -1.0235
0.4757, -0.09890, -1.0181
0.5137, -0.09070, -1.0308
0.5694, -0.07640, -0.8864
         
15 Flap element taps
1.0000, 0.00130, -1.0871
0.9365, 0.01390, 0.4005
0.8333, 0.03280, 0.2775
0.7436, 0.04930, 0.1502
0.7049, 0.05670, 0.2153
0.6662, 0.06410, 0.2927
0.6522, 0.01390, -1.0674
0.5969, -0.00020, -1.0820
0.6000, -0.03020, -1.0714
0.6324, -0.04540, -1.0721
0.6667, -0.04880, -1.0887
0.7046, -0.04110, -1.0813
0.7429, -0.03210, -1.0869
0.8333, -0.01400, -1.0935
0.9311, -0.00120, -1.0928
            
---------
         
Run Conditions: vel=220.4 ft/s  Re=2.062x10^6  AOA=27.02  Flap deflection=-90.00
Totals: Cl=0.7209  Cdp=0.2741  Cm(c/4)=-0.0471  Cs=0.0833  Ch=-0.1836
Main component: Cl=0.6226  Cdp=0.4257  Cm=-0.1866
Flap component: Cl=0.0983  Cdp=-0.1516  Cm=-0.0522
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.4910
0.6175, -0.04610, -0.6258
0.5841, -0.02440, -0.6186
0.5775, 0.01750, -0.6169
0.5777, 0.04660, -0.6102
0.6274, 0.07170, -0.9742
0.5694, 0.08320, -1.0628
0.5112, 0.09370, -1.2617
0.4731, 0.09830, -1.3738
0.4349, 0.10070, -1.3506
0.3960, 0.10120, -1.2664
0.3566, 0.10020, -1.1995
0.3172, 0.09790, -1.1427
0.2778, 0.09440, -1.1094
0.2393, 0.08960, -1.0877
0.2056, 0.08360, -1.0702
0.1633, 0.07610, -1.0680
0.1261, 0.06710, -1.0582
0.0900, 0.05640, -1.0529
0.0571, 0.04390, -1.0486
0.0283, 0.02940, -1.0493
0.0142, 0.01970, -1.0608
0.0081, 0.01410, -1.0654
0.0026, 0.00780, -0.9845
0.0000, 0.00000, -1.1123
0.0037, -0.00840, 0.1112
0.0112, -0.01420, 0.7513
0.0191, -0.01930, 0.9325
0.0397, -0.03030, 1.0115
0.0706, -0.04420, 0.9519
0.1037, -0.05710, 0.8403
0.1384, -0.06890, 0.6996
0.1741, -0.07950, 0.5599
0.2102, -0.08660, 0.4111
0.2472, -0.09640, 0.2346
0.2844, -0.10270, 0.0770
0.3225, -0.10690, -0.0972
0.3608, -0.10890, -0.2582
0.3991, -0.10830, -0.4022
0.4373, -0.10510, -0.4832
0.4757, -0.09890, -0.5014
0.5137, -0.09070, -0.5371
0.5694, -0.07640, -0.4542
         
15 Flap element taps
1.0000, 0.00130, -0.7860
0.9365, 0.01390, -1.0011
0.8333, 0.03280, -1.3424
0.7436, 0.04930, -1.0892
0.7049, 0.05670, -1.0112
0.6662, 0.06410, -0.9378
0.6522, 0.01390, -0.6208
0.5969, -0.00020, -0.6307
0.6000, -0.03020, -0.6069
0.6324, -0.04540, -0.5656
0.6667, -0.04880, -0.5504
0.7046, -0.04110, -0.5357
0.7429, -0.03210, -0.5343
0.8333, -0.01400, -0.5451
0.9311, -0.00120, -0.5667