S809 UNVENTED AILERON, LEGR, CHORD = 18 INCHES
          
---------
         
Run Conditions: vel=221.5 ft/s  Re=1.997x10^6  AOA=-6.01  Flap deflection=-60.00
Totals: Cl=-1.6396  Cdp=0.3729  Cm(c/4)=0.2007  Cs=-0.1992  Ch=0.4085
Main component: Cl=-1.4292  Cdp=-0.0056  Cm=0.3699
Flap component: Cl=-0.2104  Cdp=0.3785  Cm=0.2482
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.7670
0.6175, -0.04610, -0.7446
0.5841, -0.02440, -0.7403
0.5775, 0.01750, -0.7410
0.5777, 0.04660, -0.7404
0.6274, 0.07170, 0.8471
0.5694, 0.08320, 0.8437
0.5112, 0.09370, 0.7612
0.4731, 0.09830, 0.6621
0.4349, 0.10070, 0.6223
0.3960, 0.10120, 0.5980
0.3566, 0.10020, 0.5870
0.3172, 0.09790, 0.5954
0.2778, 0.09440, 0.6075
0.2393, 0.08960, 0.6334
0.2056, 0.08360, 0.6761
0.1633, 0.07610, 0.7383
0.1261, 0.06710, 0.8168
0.0900, 0.05640, 0.9074
0.0571, 0.04390, 0.9952
0.0283, 0.02940, 0.9617
0.0142, 0.01970, 0.6496
0.0081, 0.01410, 0.1790
0.0026, 0.00780, -1.0995
0.0000, 0.00000, -5.8992
0.0037, -0.00840, -6.4215
0.0112, -0.01420, -4.4106
0.0191, -0.01930, -3.4703
0.0397, -0.03030, -2.5937
0.0706, -0.04420, -2.1475
0.1037, -0.05710, -1.8937
0.1384, -0.06890, -1.8707
0.1741, -0.07950, -1.8174
0.2102, -0.08660, -1.8154
0.2472, -0.09640, -1.8362
0.2844, -0.10270, -1.7872
0.3225, -0.10690, -1.7122
0.3608, -0.10890, -1.5917
0.3991, -0.10830, -1.3706
0.4373, -0.10510, -1.0857
0.4757, -0.09890, -0.8725
0.5137, -0.09070, -0.8065
0.5694, -0.07640, -0.7876
         
15 Flap element taps
1.0000, 0.00130, -0.7432
0.9365, 0.01390, 0.2883
0.8333, 0.03280, 0.6648
0.7436, 0.04930, 0.8521
0.7049, 0.05670, 0.8938
0.6662, 0.06410, 0.8526
0.6522, 0.01390, -0.7410
0.5969, -0.00020, -0.7502
0.6000, -0.03020, -0.7499
0.6324, -0.04540, -0.7532
0.6667, -0.04880, -0.7545
0.7046, -0.04110, -0.7484
0.7429, -0.03210, -0.7488
0.8333, -0.01400, -0.7495
0.9311, -0.00120, -0.7410
            
---------
         
Run Conditions: vel=222.4 ft/s  Re=1.998x10^6  AOA=-0.03  Flap deflection=-60.00
Totals: Cl=-1.5171  Cdp=0.2913  Cm(c/4)=0.2222  Cs=-0.2905  Ch=0.3781
Main component: Cl=-1.2900  Cdp=-0.0295  Cm=0.3742
Flap component: Cl=-0.2270  Cdp=0.3208  Cm=0.2273
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.7382
0.6175, -0.04610, -0.6915
0.5841, -0.02440, -0.6870
0.5775, 0.01750, -0.6902
0.5777, 0.04660, -0.6894
0.6274, 0.07170, 0.7135
0.5694, 0.08320, 0.7217
0.5112, 0.09370, 0.7251
0.4731, 0.09830, 0.6899
0.4349, 0.10070, 0.5963
0.3960, 0.10120, 0.5312
0.3566, 0.10020, 0.4920
0.3172, 0.09790, 0.4798
0.2778, 0.09440, 0.4712
0.2393, 0.08960, 0.4725
0.2056, 0.08360, 0.4987
0.1633, 0.07610, 0.5485
0.1261, 0.06710, 0.6222
0.0900, 0.05640, 0.7085
0.0571, 0.04390, 0.8518
0.0283, 0.02940, 0.9983
0.0142, 0.01970, 0.9823
0.0081, 0.01410, 0.8369
0.0026, 0.00780, 0.0938
0.0000, 0.00000, -2.2882
0.0037, -0.00840, -3.4568
0.0112, -0.01420, -2.5577
0.0191, -0.01930, -1.9080
0.0397, -0.03030, -1.5545
0.0706, -0.04420, -1.4540
0.1037, -0.05710, -1.3279
0.1384, -0.06890, -1.4573
0.1741, -0.07950, -1.5060
0.2102, -0.08660, -1.5919
0.2472, -0.09640, -1.7143
0.2844, -0.10270, -1.7653
0.3225, -0.10690, -1.8057
0.3608, -0.10890, -1.8253
0.3991, -0.10830, -1.7592
0.4373, -0.10510, -1.6102
0.4757, -0.09890, -1.3474
0.5137, -0.09070, -1.1052
0.5694, -0.07640, -0.8400
         
15 Flap element taps
1.0000, 0.00130, -0.6901
0.9365, 0.01390, 0.2701
0.8333, 0.03280, 0.6530
0.7436, 0.04930, 0.7295
0.7049, 0.05670, 0.7138
0.6662, 0.06410, 0.7104
0.6522, 0.01390, -0.6893
0.5969, -0.00020, -0.6936
0.6000, -0.03020, -0.6908
0.6324, -0.04540, -0.6888
0.6667, -0.04880, -0.6880
0.7046, -0.04110, -0.6842
0.7429, -0.03210, -0.6887
0.8333, -0.01400, -0.6914
0.9311, -0.00120, -0.6869
            
---------
         
Run Conditions: vel=223.2 ft/s  Re=1.998x10^6  AOA=3.01  Flap deflection=-60.00
Totals: Cl=-1.5039  Cdp=0.2831  Cm(c/4)=0.2495  Cs=-0.3616  Ch=0.3971
Main component: Cl=-1.2492  Cdp=-0.0385  Cm=0.3834
Flap component: Cl=-0.2547  Cdp=0.3215  Cm=0.2379
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.8658
0.6175, -0.04610, -0.7744
0.5841, -0.02440, -0.7702
0.5775, 0.01750, -0.7707
0.5777, 0.04660, -0.7706
0.6274, 0.07170, 0.6748
0.5694, 0.08320, 0.6802
0.5112, 0.09370, 0.6880
0.4731, 0.09830, 0.6684
0.4349, 0.10070, 0.5792
0.3960, 0.10120, 0.5018
0.3566, 0.10020, 0.4497
0.3172, 0.09790, 0.4285
0.2778, 0.09440, 0.4124
0.2393, 0.08960, 0.4056
0.2056, 0.08360, 0.4210
0.1633, 0.07610, 0.4600
0.1261, 0.06710, 0.5258
0.0900, 0.05640, 0.6002
0.0571, 0.04390, 0.7504
0.0283, 0.02940, 0.9443
0.0142, 0.01970, 1.0126
0.0081, 0.01410, 0.9631
0.0026, 0.00780, 0.4517
0.0000, 0.00000, -1.1579
0.0037, -0.00840, -2.4067
0.0112, -0.01420, -1.8588
0.0191, -0.01930, -1.3908
0.0397, -0.03030, -1.1949
0.0706, -0.04420, -1.2005
0.1037, -0.05710, -1.1240
0.1384, -0.06890, -1.3038
0.1741, -0.07950, -1.3878
0.2102, -0.08660, -1.5073
0.2472, -0.09640, -1.6670
0.2844, -0.10270, -1.7518
0.3225, -0.10690, -1.8337
0.3608, -0.10890, -1.8965
0.3991, -0.10830, -1.8784
0.4373, -0.10510, -1.7820
0.4757, -0.09890, -1.5663
0.5137, -0.09070, -1.3572
0.5694, -0.07640, -1.0588
         
15 Flap element taps
1.0000, 0.00130, -0.7678
0.9365, 0.01390, 0.2483
0.8333, 0.03280, 0.6436
0.7436, 0.04930, 0.6902
0.7049, 0.05670, 0.6736
0.6662, 0.06410, 0.6741
0.6522, 0.01390, -0.7700
0.5969, -0.00020, -0.7741
0.6000, -0.03020, -0.7712
0.6324, -0.04540, -0.7671
0.6667, -0.04880, -0.7650
0.7046, -0.04110, -0.7640
0.7429, -0.03210, -0.7707
0.8333, -0.01400, -0.7756
0.9311, -0.00120, -0.7643
            
---------
         
Run Conditions: vel=222.5 ft/s  Re=1.988x10^6  AOA=6.02  Flap deflection=-60.00
Totals: Cl=-1.3089  Cdp=0.2649  Cm(c/4)=0.2538  Cs=-0.4007  Ch=0.3855
Main component: Cl=-1.0471  Cdp=-0.0307  Cm=0.3424
Flap component: Cl=-0.2617  Cdp=0.2957  Cm=0.2299
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.8626
0.6175, -0.04610, -0.7660
0.5841, -0.02440, -0.7653
0.5775, 0.01750, -0.7670
0.5777, 0.04660, -0.7662
0.6274, 0.07170, 0.6165
0.5694, 0.08320, 0.6219
0.5112, 0.09370, 0.6321
0.4731, 0.09830, 0.6265
0.4349, 0.10070, 0.5574
0.3960, 0.10120, 0.4595
0.3566, 0.10020, 0.3857
0.3172, 0.09790, 0.3477
0.2778, 0.09440, 0.3159
0.2393, 0.08960, 0.2922
0.2056, 0.08360, 0.2908
0.1633, 0.07610, 0.3125
0.1261, 0.06710, 0.3615
0.0900, 0.05640, 0.4197
0.0571, 0.04390, 0.5486
0.0283, 0.02940, 0.7762
0.0142, 0.01970, 0.9357
0.0081, 0.01410, 1.0032
0.0026, 0.00780, 0.7734
0.0000, 0.00000, 0.1546
0.0037, -0.00840, -0.9879
0.0112, -0.01420, -0.8621
0.0191, -0.01930, -0.6409
0.0397, -0.03030, -0.6406
0.0706, -0.04420, -0.7584
0.1037, -0.05710, -0.7494
0.1384, -0.06890, -0.9699
0.1741, -0.07950, -1.0864
0.2102, -0.08660, -1.2298
0.2472, -0.09640, -1.4111
0.2844, -0.10270, -1.5202
0.3225, -0.10690, -1.6296
0.3608, -0.10890, -1.7189
0.3991, -0.10830, -1.7330
0.4373, -0.10510, -1.6737
0.4757, -0.09890, -1.4963
0.5137, -0.09070, -1.3211
0.5694, -0.07640, -1.0379
         
15 Flap element taps
1.0000, 0.00130, -0.7542
0.9365, 0.01390, 0.2340
0.8333, 0.03280, 0.6277
0.7436, 0.04930, 0.6212
0.7049, 0.05670, 0.6069
0.6662, 0.06410, 0.6149
0.6522, 0.01390, -0.7616
0.5969, -0.00020, -0.7684
0.6000, -0.03020, -0.7632
0.6324, -0.04540, -0.7534
0.6667, -0.04880, -0.7515
0.7046, -0.04110, -0.7501
0.7429, -0.03210, -0.7558
0.8333, -0.01400, -0.7642
0.9311, -0.00120, -0.7548
            
---------
         
Run Conditions: vel=223.5 ft/s  Re=1.994x10^6  AOA=9.03  Flap deflection=-60.00
Totals: Cl=-1.0972  Cdp=0.2554  Cm(c/4)=0.2566  Cs=-0.4244  Ch=0.3763
Main component: Cl=-0.8288  Cdp=-0.0165  Cm=0.2941
Flap component: Cl=-0.2684  Cdp=0.2718  Cm=0.2234
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.8450
0.6175, -0.04610, -0.7706
0.5841, -0.02440, -0.7662
0.5775, 0.01750, -0.7705
0.5777, 0.04660, -0.7708
0.6274, 0.07170, 0.5494
0.5694, 0.08320, 0.5500
0.5112, 0.09370, 0.5594
0.4731, 0.09830, 0.5620
0.4349, 0.10070, 0.5271
0.3960, 0.10120, 0.4238
0.3566, 0.10020, 0.3230
0.3172, 0.09790, 0.2643
0.2778, 0.09440, 0.2135
0.2393, 0.08960, 0.1684
0.2056, 0.08360, 0.1464
0.1633, 0.07610, 0.1440
0.1261, 0.06710, 0.1691
0.0900, 0.05640, 0.2167
0.0571, 0.04390, 0.2811
0.0283, 0.02940, 0.4935
0.0142, 0.01970, 0.6666
0.0081, 0.01410, 0.8313
0.0026, 0.00780, 0.9020
0.0000, 0.00000, 0.8806
0.0037, -0.00840, 0.0953
0.0112, -0.01420, -0.0502
0.0191, -0.01930, -0.0193
0.0397, -0.03030, -0.1495
0.0706, -0.04420, -0.3446
0.1037, -0.05710, -0.3938
0.1384, -0.06890, -0.6407
0.1741, -0.07950, -0.7809
0.2102, -0.08660, -0.9411
0.2472, -0.09640, -1.1378
0.2844, -0.10270, -1.2665
0.3225, -0.10690, -1.3993
0.3608, -0.10890, -1.5105
0.3991, -0.10830, -1.5534
0.4373, -0.10510, -1.5268
0.4757, -0.09890, -1.3840
0.5137, -0.09070, -1.2455
0.5694, -0.07640, -0.9918
         
15 Flap element taps
1.0000, 0.00130, -0.7578
0.9365, 0.01390, 0.2215
0.8333, 0.03280, 0.5944
0.7436, 0.04930, 0.5480
0.7049, 0.05670, 0.5364
0.6662, 0.06410, 0.5462
0.6522, 0.01390, -0.7657
0.5969, -0.00020, -0.7718
0.6000, -0.03020, -0.7672
0.6324, -0.04540, -0.7557
0.6667, -0.04880, -0.7532
0.7046, -0.04110, -0.7521
0.7429, -0.03210, -0.7576
0.8333, -0.01400, -0.7652
0.9311, -0.00120, -0.7592
            
---------
         
Run Conditions: vel=224.4 ft/s  Re=1.996x10^6  AOA=12.02  Flap deflection=-60.00
Totals: Cl=-0.8693  Cdp=0.2460  Cm(c/4)=0.2563  Cs=-0.4217  Ch=0.3640
Main component: Cl=-0.5989  Cdp=0.0004  Cm=0.2413
Flap component: Cl=-0.2705  Cdp=0.2456  Cm=0.2147
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.8128
0.6175, -0.04610, -0.7666
0.5841, -0.02440, -0.7614
0.5775, 0.01750, -0.7637
0.5777, 0.04660, -0.7641
0.6274, 0.07170, 0.4610
0.5694, 0.08320, 0.4601
0.5112, 0.09370, 0.4723
0.4731, 0.09830, 0.4783
0.4349, 0.10070, 0.4673
0.3960, 0.10120, 0.3913
0.3566, 0.10020, 0.2683
0.3172, 0.09790, 0.1841
0.2778, 0.09440, 0.1079
0.2393, 0.08960, 0.0385
0.2056, 0.08360, -0.0097
0.1633, 0.07610, -0.0431
0.1261, 0.06710, -0.0508
0.0900, 0.05640, -0.0395
0.0571, 0.04390, -0.0534
0.0283, 0.02940, 0.0874
0.0142, 0.01970, 0.1790
0.0081, 0.01410, 0.3934
0.0026, 0.00780, 0.5841
0.0000, 0.00000, 0.9923
0.0037, -0.00840, 0.7881
0.0112, -0.01420, 0.5162
0.0191, -0.01930, 0.4611
0.0397, -0.03030, 0.2679
0.0706, -0.04420, 0.0315
0.1037, -0.05710, -0.0671
0.1384, -0.06890, -0.3244
0.1741, -0.07950, -0.4838
0.2102, -0.08660, -0.6565
0.2472, -0.09640, -0.8623
0.2844, -0.10270, -1.0073
0.3225, -0.10690, -1.1577
0.3608, -0.10890, -1.2869
0.3991, -0.10830, -1.3555
0.4373, -0.10510, -1.3585
0.4757, -0.09890, -1.2492
0.5137, -0.09070, -1.1550
0.5694, -0.07640, -0.9278
         
15 Flap element taps
1.0000, 0.00130, -0.7559
0.9365, 0.01390, 0.2123
0.8333, 0.03280, 0.5553
0.7436, 0.04930, 0.4605
0.7049, 0.05670, 0.4508
0.6662, 0.06410, 0.4605
0.6522, 0.01390, -0.7619
0.5969, -0.00020, -0.7693
0.6000, -0.03020, -0.7655
0.6324, -0.04540, -0.7520
0.6667, -0.04880, -0.7492
0.7046, -0.04110, -0.7499
0.7429, -0.03210, -0.7547
0.8333, -0.01400, -0.7632
0.9311, -0.00120, -0.7546
            
---------
         
Run Conditions: vel=225.4 ft/s  Re=1.996x10^6  AOA=15.00  Flap deflection=-60.00
Totals: Cl=-0.6169  Cdp=0.2312  Cm(c/4)=0.2468  Cs=-0.3830  Ch=0.3375
Main component: Cl=-0.3583  Cdp=0.0210  Cm=0.1836
Flap component: Cl=-0.2586  Cdp=0.2102  Cm=0.1972
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.7626
0.6175, -0.04610, -0.7531
0.5841, -0.02440, -0.7458
0.5775, 0.01750, -0.7427
0.5777, 0.04660, -0.7432
0.6274, 0.07170, 0.3529
0.5694, 0.08320, 0.3424
0.5112, 0.09370, 0.3563
0.4731, 0.09830, 0.3667
0.4349, 0.10070, 0.3659
0.3960, 0.10120, 0.3422
0.3566, 0.10020, 0.2477
0.3172, 0.09790, 0.1294
0.2778, 0.09440, 0.0143
0.2393, 0.08960, -0.0861
0.2056, 0.08360, -0.1692
0.1633, 0.07610, -0.2433
0.1261, 0.06710, -0.2936
0.0900, 0.05640, -0.3347
0.0571, 0.04390, -0.4464
0.0283, 0.02940, -0.4346
0.0142, 0.01970, -0.5164
0.0081, 0.01410, -0.3359
0.0026, 0.00780, -0.0965
0.0000, 0.00000, 0.4390
0.0037, -0.00840, 1.0088
0.0112, -0.01420, 0.9174
0.0191, -0.01930, 0.8038
0.0397, -0.03030, 0.6046
0.0706, -0.04420, 0.3572
0.1037, -0.05710, 0.2178
0.1384, -0.06890, -0.0255
0.1741, -0.07950, -0.1975
0.2102, -0.08660, -0.3761
0.2472, -0.09640, -0.5849
0.2844, -0.10270, -0.7417
0.3225, -0.10690, -0.9058
0.3608, -0.10890, -1.0513
0.3991, -0.10830, -1.1409
0.4373, -0.10510, -1.1684
0.4757, -0.09890, -1.0893
0.5137, -0.09070, -1.0373
0.5694, -0.07640, -0.8453
         
15 Flap element taps
1.0000, 0.00130, -0.7326
0.9365, 0.01390, 0.2119
0.8333, 0.03280, 0.4607
0.7436, 0.04930, 0.3325
0.7049, 0.05670, 0.3308
0.6662, 0.06410, 0.3487
0.6522, 0.01390, -0.7386
0.5969, -0.00020, -0.7474
0.6000, -0.03020, -0.7450
0.6324, -0.04540, -0.7337
0.6667, -0.04880, -0.7274
0.7046, -0.04110, -0.7282
0.7429, -0.03210, -0.7347
0.8333, -0.01400, -0.7366
0.9311, -0.00120, -0.7304
            
---------
         
Run Conditions: vel=226.8 ft/s  Re=2.004x10^6  AOA=17.99  Flap deflection=-60.00
Totals: Cl=-0.3330  Cdp=0.2153  Cm(c/4)=0.2257  Cs=-0.3076  Ch=0.3011
Main component: Cl=-0.1003  Cdp=0.0482  Cm=0.1159
Flap component: Cl=-0.2327  Cdp=0.1671  Cm=0.1724
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.6907
0.6175, -0.04610, -0.7073
0.5841, -0.02440, -0.7025
0.5775, 0.01750, -0.7100
0.5777, 0.04660, -0.7091
0.6274, 0.07170, 0.1684
0.5694, 0.08320, 0.1475
0.5112, 0.09370, 0.1677
0.4731, 0.09830, 0.1808
0.4349, 0.10070, 0.1850
0.3960, 0.10120, 0.1847
0.3566, 0.10020, 0.1612
0.3172, 0.09790, 0.0898
0.2778, 0.09440, -0.0398
0.2393, 0.08960, -0.1786
0.2056, 0.08360, -0.3080
0.1633, 0.07610, -0.4345
0.1261, 0.06710, -0.5418
0.0900, 0.05640, -0.6630
0.0571, 0.04390, -0.8897
0.0283, 0.02940, -1.0613
0.0142, 0.01970, -1.4099
0.0081, 0.01410, -1.3257
0.0026, 0.00780, -1.0909
0.0000, 0.00000, -0.9881
0.0037, -0.00840, 0.8021
0.0112, -0.01420, 1.0101
0.0191, -0.01930, 0.9851
0.0397, -0.03030, 0.8407
0.0706, -0.04420, 0.6222
0.1037, -0.05710, 0.4548
0.1384, -0.06890, 0.2416
0.1741, -0.07950, 0.0668
0.2102, -0.08660, -0.1097
0.2472, -0.09640, -0.3152
0.2844, -0.10270, -0.4777
0.3225, -0.10690, -0.6495
0.3608, -0.10890, -0.8038
0.3991, -0.10830, -0.9119
0.4373, -0.10510, -0.9611
0.4757, -0.09890, -0.9112
0.5137, -0.09070, -0.8943
0.5694, -0.07640, -0.7318
         
15 Flap element taps
1.0000, 0.00130, -0.6976
0.9365, 0.01390, 0.2197
0.8333, 0.03280, 0.3441
0.7436, 0.04930, 0.1551
0.7049, 0.05670, 0.1426
0.6662, 0.06410, 0.1743
0.6522, 0.01390, -0.7031
0.5969, -0.00020, -0.7122
0.6000, -0.03020, -0.7087
0.6324, -0.04540, -0.6920
0.6667, -0.04880, -0.6865
0.7046, -0.04110, -0.6878
0.7429, -0.03210, -0.6911
0.8333, -0.01400, -0.6965
0.9311, -0.00120, -0.6904
            
---------
         
Run Conditions: vel=227.6 ft/s  Re=2.006x10^6  AOA=19.99  Flap deflection=-60.00
Totals: Cl=-0.0860  Cdp=0.2009  Cm(c/4)=0.1900  Cs=-0.2182  Ch=0.2468
Main component: Cl=0.1000  Cdp=0.0799  Cm=0.0562
Flap component: Cl=-0.1860  Cdp=0.1210  Cm=0.1369
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.6232
0.6175, -0.04610, -0.6635
0.5841, -0.02440, -0.6621
0.5775, 0.01750, -0.6668
0.5777, 0.04660, -0.6659
0.6274, 0.07170, -0.0357
0.5694, 0.08320, -0.0798
0.5112, 0.09370, -0.0455
0.4731, 0.09830, -0.0387
0.4349, 0.10070, -0.0315
0.3960, 0.10120, -0.0266
0.3566, 0.10020, -0.0366
0.3172, 0.09790, -0.0463
0.2778, 0.09440, -0.0820
0.2393, 0.08960, -0.1775
0.2056, 0.08360, -0.3315
0.1633, 0.07610, -0.5125
0.1261, 0.06710, -0.6822
0.0900, 0.05640, -0.8841
0.0571, 0.04390, -1.2031
0.0283, 0.02940, -1.5462
0.0142, 0.01970, -2.1259
0.0081, 0.01410, -2.1813
0.0026, 0.00780, -1.9499
0.0000, 0.00000, -2.5007
0.0037, -0.00840, 0.3950
0.0112, -0.01420, 0.9515
0.0191, -0.01930, 1.0091
0.0397, -0.03030, 0.9474
0.0706, -0.04420, 0.7705
0.1037, -0.05710, 0.6122
0.1384, -0.06890, 0.4118
0.1741, -0.07950, 0.2396
0.2102, -0.08660, 0.0653
0.2472, -0.09640, -0.1359
0.2844, -0.10270, -0.2929
0.3225, -0.10690, -0.4639
0.3608, -0.10890, -0.6234
0.3991, -0.10830, -0.7396
0.4373, -0.10510, -0.8001
0.4757, -0.09890, -0.7696
0.5137, -0.09070, -0.7820
0.5694, -0.07640, -0.6412
         
15 Flap element taps
1.0000, 0.00130, -0.6496
0.9365, 0.01390, 0.2085
0.8333, 0.03280, 0.1421
0.7436, 0.04930, -0.0653
0.7049, 0.05670, -0.0776
0.6662, 0.06410, -0.0295
0.6522, 0.01390, -0.6608
0.5969, -0.00020, -0.6683
0.6000, -0.03020, -0.6629
0.6324, -0.04540, -0.6415
0.6667, -0.04880, -0.6342
0.7046, -0.04110, -0.6373
0.7429, -0.03210, -0.6395
0.8333, -0.01400, -0.6449
0.9311, -0.00120, -0.6424
            
---------
         
Run Conditions: vel=226.6 ft/s  Re=1.997x10^6  AOA=24.02  Flap deflection=-60.00
Totals: Cl=0.5564  Cdp=0.2314  Cm(c/4)=0.0060  Cs=0.0151  Ch=-0.0378
Main component: Cl=0.5009  Cdp=0.2879  Cm=-0.1163
Flap component: Cl=0.0556  Cdp=-0.0565  Cm=-0.0284
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.5606
0.6175, -0.04610, -0.7505
0.5841, -0.02440, -0.7478
0.5775, 0.01750, -0.7563
0.5777, 0.04660, -0.7548
0.6274, 0.07170, -0.6858
0.5694, 0.08320, -0.8309
0.5112, 0.09370, -0.8553
0.4731, 0.09830, -0.8507
0.4349, 0.10070, -0.8363
0.3960, 0.10120, -0.8318
0.3566, 0.10020, -0.8443
0.3172, 0.09790, -0.8552
0.2778, 0.09440, -0.8583
0.2393, 0.08960, -0.8587
0.2056, 0.08360, -0.8649
0.1633, 0.07610, -0.8923
0.1261, 0.06710, -0.9147
0.0900, 0.05640, -0.9471
0.0571, 0.04390, -1.0241
0.0283, 0.02940, -1.2271
0.0142, 0.01970, -1.7507
0.0081, 0.01410, -2.1285
0.0026, 0.00780, -2.1699
0.0000, 0.00000, -3.9726
0.0037, -0.00840, -0.2957
0.0112, -0.01420, 0.7317
0.0191, -0.01930, 0.9235
0.0397, -0.03030, 1.0114
0.0706, -0.04420, 0.9314
0.1037, -0.05710, 0.8147
0.1384, -0.06890, 0.6496
0.1741, -0.07950, 0.5008
0.2102, -0.08660, 0.3441
0.2472, -0.09640, 0.1591
0.2844, -0.10270, -0.0011
0.3225, -0.10690, -0.1793
0.3608, -0.10890, -0.3398
0.3991, -0.10830, -0.4791
0.4373, -0.10510, -0.5535
0.4757, -0.09890, -0.5549
0.5137, -0.09070, -0.5899
0.5694, -0.07640, -0.4991
         
15 Flap element taps
1.0000, 0.00130, -0.5787
0.9365, 0.01390, -0.4378
0.8333, 0.03280, -0.6804
0.7436, 0.04930, -0.7745
0.7049, 0.05670, -0.7518
0.6662, 0.06410, -0.6740
0.6522, 0.01390, -0.7441
0.5969, -0.00020, -0.7549
0.6000, -0.03020, -0.5676
0.6324, -0.04540, -0.4426
0.6667, -0.04880, -0.4296
0.7046, -0.04110, -0.4339
0.7429, -0.03210, -0.4344
0.8333, -0.01400, -0.4410
0.9311, -0.00120, -0.4576
            
---------
         
Run Conditions: vel=227.9 ft/s  Re=2.005x10^6  AOA=27.01  Flap deflection=-60.00
Totals: Cl=0.5722  Cdp=0.2931  Cm(c/4)=-0.0203  Cs=-0.0012  Ch=-0.0869
Main component: Cl=0.4765  Cdp=0.3726  Cm=-0.1285
Flap component: Cl=0.0957  Cdp=-0.0795  Cm=-0.0525
         
Surface Pressure Data
43 Main element taps 
0.6276, -0.06090, -0.6665
0.6175, -0.04610, -0.9774
0.5841, -0.02440, -0.9679
0.5775, 0.01750, -0.9716
0.5777, 0.04660, -0.9705
0.6274, 0.07170, -0.7881
0.5694, 0.08320, -0.8910
0.5112, 0.09370, -0.9241
0.4731, 0.09830, -0.9418
0.4349, 0.10070, -0.9289
0.3960, 0.10120, -0.9094
0.3566, 0.10020, -0.9114
0.3172, 0.09790, -0.9039
0.2778, 0.09440, -0.9004
0.2393, 0.08960, -0.8951
0.2056, 0.08360, -0.8886
0.1633, 0.07610, -0.9019
0.1261, 0.06710, -0.9095
0.0900, 0.05640, -0.9359
0.0571, 0.04390, -0.9693
0.0283, 0.02940, -1.0309
0.0142, 0.01970, -1.1834
0.0081, 0.01410, -1.4095
0.0026, 0.00780, -1.4430
0.0000, 0.00000, -3.2241
0.0037, -0.00840, -0.2280
0.0112, -0.01420, 0.7202
0.0191, -0.01930, 0.9079
0.0397, -0.03030, 1.0106
0.0706, -0.04420, 0.9510
0.1037, -0.05710, 0.8471
0.1384, -0.06890, 0.6930
0.1741, -0.07950, 0.5503
0.2102, -0.08660, 0.3979
0.2472, -0.09640, 0.2141
0.2844, -0.10270, 0.0510
0.3225, -0.10690, -0.1323
0.3608, -0.10890, -0.3025
0.3991, -0.10830, -0.4548
0.4373, -0.10510, -0.5468
0.4757, -0.09890, -0.5697
0.5137, -0.09070, -0.6234
0.5694, -0.07640, -0.5607
         
15 Flap element taps
1.0000, 0.00130, -0.8360
0.9365, 0.01390, -0.7932
0.8333, 0.03280, -0.9014
0.7436, 0.04930, -0.8923
0.7049, 0.05670, -0.8518
0.6662, 0.06410, -0.8051
0.6522, 0.01390, -0.9693
0.5969, -0.00020, -0.9820
0.6000, -0.03020, -0.7153
0.6324, -0.04540, -0.5322
0.6667, -0.04880, -0.5055
0.7046, -0.04110, -0.5127
0.7429, -0.03210, -0.5140
0.8333, -0.01400, -0.5317
0.9311, -0.00120, -0.5588