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WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA) (fx6617ai-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA) (fx6617ai-il)
Reynolds number: 1,000,000
Max Cl/Cd: 130.67 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx6617ai-il-1000000-n5.txt
Download as CSV file: xf-fx6617ai-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT N
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7885   0.12011   0.11784  -0.0305   0.9998   0.0076
 -18.250  -0.8268   0.10868   0.10624  -0.0365   0.9998   0.0076
 -18.000  -0.8573   0.09900   0.09642  -0.0417   0.9998   0.0076
 -17.750  -0.8818   0.09071   0.08799  -0.0462   0.9998   0.0076
 -17.500  -0.9001   0.08363   0.08040  -0.0505   0.8446   0.0076
 -17.250  -0.9162   0.07761   0.07399  -0.0536   0.7753   0.0076
 -17.000  -0.9292   0.07192   0.06807  -0.0567   0.7462   0.0077
 -16.750  -0.9446   0.06611   0.06206  -0.0599   0.7245   0.0077
 -16.500  -0.9564   0.06103   0.05679  -0.0626   0.7046   0.0078
 -16.250  -0.9644   0.05661   0.05221  -0.0649   0.6872   0.0079
 -15.750  -0.9714   0.04948   0.04480  -0.0683   0.6596   0.0081
 -15.500  -0.9722   0.04652   0.04172  -0.0695   0.6492   0.0081
 -15.250  -0.9705   0.04389   0.03898  -0.0706   0.6394   0.0082
 -15.000  -0.9669   0.04152   0.03651  -0.0714   0.6306   0.0083
 -14.750  -0.9618   0.03935   0.03424  -0.0722   0.6228   0.0084
 -14.500  -0.9554   0.03734   0.03214  -0.0729   0.6156   0.0085
 -14.250  -0.9476   0.03550   0.03020  -0.0734   0.6090   0.0086
 -14.000  -0.9387   0.03377   0.02839  -0.0740   0.6039   0.0087
 -13.750  -0.9288   0.03215   0.02669  -0.0744   0.5987   0.0088
 -13.250  -0.9061   0.02918   0.02355  -0.0752   0.5901   0.0091
 -13.000  -0.8933   0.02782   0.02211  -0.0756   0.5861   0.0092
 -12.750  -0.8796   0.02653   0.02074  -0.0760   0.5821   0.0094
 -12.250  -0.8494   0.02415   0.01819  -0.0768   0.5749   0.0097
 -12.000  -0.8328   0.02305   0.01701  -0.0774   0.5715   0.0098
 -11.750  -0.8165   0.02202   0.01590  -0.0778   0.5679   0.0099
 -11.500  -0.8000   0.02121   0.01499  -0.0778   0.5646   0.0100
 -11.000  -0.7583   0.01994   0.01358  -0.0779   0.5593   0.0102
 -10.750  -0.7383   0.01915   0.01272  -0.0778   0.5568   0.0104
 -10.500  -0.7177   0.01838   0.01189  -0.0777   0.5542   0.0107
 -10.250  -0.6951   0.01779   0.01125  -0.0777   0.5516   0.0109
 -10.000  -0.6716   0.01729   0.01069  -0.0778   0.5490   0.0112
  -9.750  -0.6475   0.01682   0.01016  -0.0778   0.5463   0.0113
  -9.500  -0.6229   0.01637   0.00967  -0.0779   0.5442   0.0115
  -9.250  -0.5979   0.01593   0.00918  -0.0780   0.5419   0.0117
  -9.000  -0.5727   0.01551   0.00872  -0.0780   0.5395   0.0119
  -8.750  -0.5472   0.01510   0.00826  -0.0781   0.5371   0.0122
  -8.500  -0.5215   0.01472   0.00782  -0.0782   0.5348   0.0124
  -8.250  -0.4954   0.01437   0.00742  -0.0784   0.5326   0.0126
  -7.750  -0.4422   0.01376   0.00673  -0.0787   0.5288   0.0132
  -7.500  -0.4151   0.01349   0.00642  -0.0789   0.5271   0.0134
  -7.250  -0.3889   0.01307   0.00596  -0.0790   0.5252   0.0139
  -7.000  -0.3620   0.01274   0.00560  -0.0792   0.5231   0.0144
  -6.750  -0.3348   0.01247   0.00529  -0.0794   0.5209   0.0149
  -6.500  -0.3074   0.01222   0.00501  -0.0796   0.5186   0.0154
  -6.250  -0.2798   0.01201   0.00475  -0.0798   0.5165   0.0160
  -6.000  -0.2521   0.01181   0.00452  -0.0800   0.5146   0.0166
  -5.750  -0.2240   0.01161   0.00429  -0.0803   0.5133   0.0172
  -5.500  -0.1961   0.01138   0.00406  -0.0806   0.5117   0.0186
  -5.250  -0.1680   0.01119   0.00386  -0.0808   0.5101   0.0202
  -5.000  -0.1397   0.01102   0.00368  -0.0811   0.5084   0.0219
  -4.750  -0.1115   0.01084   0.00349  -0.0814   0.5065   0.0254
  -4.500  -0.0833   0.01068   0.00333  -0.0817   0.5046   0.0298
  -4.250  -0.0550   0.01053   0.00317  -0.0820   0.5026   0.0353
  -4.000  -0.0269   0.01036   0.00301  -0.0823   0.5006   0.0442
  -3.750   0.0008   0.01007   0.00283  -0.0826   0.4991   0.0720
  -3.500   0.0286   0.00978   0.00266  -0.0829   0.4978   0.1068
  -3.250   0.0559   0.00938   0.00246  -0.0832   0.4965   0.1640
  -3.000   0.0826   0.00886   0.00224  -0.0835   0.4950   0.2482
  -2.750   0.1087   0.00826   0.00201  -0.0838   0.4935   0.3531
  -2.500   0.1361   0.00792   0.00191  -0.0841   0.4919   0.4313
  -2.250   0.1650   0.00784   0.00187  -0.0845   0.4902   0.4555
  -2.000   0.1937   0.00776   0.00185  -0.0848   0.4884   0.4834
  -1.750   0.2225   0.00771   0.00185  -0.0851   0.4866   0.5082
  -1.500   0.2516   0.00773   0.00185  -0.0855   0.4847   0.5195
  -1.250   0.2810   0.00773   0.00185  -0.0859   0.4836   0.5270
  -1.000   0.3105   0.00774   0.00185  -0.0863   0.4825   0.5348
  -0.750   0.3399   0.00774   0.00187  -0.0867   0.4812   0.5422
  -0.500   0.3694   0.00777   0.00188  -0.0872   0.4798   0.5492
  -0.250   0.3987   0.00779   0.00190  -0.0876   0.4783   0.5552
   0.000   0.4280   0.00782   0.00192  -0.0880   0.4767   0.5603
   0.250   0.4574   0.00786   0.00194  -0.0884   0.4750   0.5640
   0.500   0.4866   0.00789   0.00196  -0.0888   0.4734   0.5677
   0.750   0.5157   0.00794   0.00200  -0.0892   0.4717   0.5716
   1.000   0.5447   0.00800   0.00204  -0.0896   0.4701   0.5753
   1.250   0.5740   0.00804   0.00208  -0.0901   0.4690   0.5786
   1.500   0.6034   0.00808   0.00212  -0.0905   0.4680   0.5815
   1.750   0.6327   0.00811   0.00217  -0.0909   0.4667   0.5848
   2.000   0.6619   0.00814   0.00223  -0.0914   0.4653   0.5883
   2.250   0.6910   0.00819   0.00228  -0.0918   0.4637   0.5917
   2.500   0.7202   0.00824   0.00233  -0.0922   0.4620   0.5947
   2.750   0.7492   0.00830   0.00239  -0.0926   0.4605   0.5972
   3.000   0.7780   0.00835   0.00246  -0.0930   0.4591   0.6000
   3.250   0.8068   0.00842   0.00253  -0.0934   0.4577   0.6031
   3.500   0.8354   0.00850   0.00262  -0.0938   0.4561   0.6063
   3.750   0.8641   0.00857   0.00271  -0.0941   0.4546   0.6094
   4.000   0.8932   0.00863   0.00279  -0.0946   0.4534   0.6120
   4.250   0.9221   0.00868   0.00288  -0.0950   0.4520   0.6144
   4.500   0.9508   0.00873   0.00297  -0.0954   0.4507   0.6172
   4.750   0.9795   0.00880   0.00307  -0.0958   0.4492   0.6204
   5.000   1.0081   0.00887   0.00318  -0.0962   0.4476   0.6234
   5.250   1.0366   0.00895   0.00328  -0.0965   0.4459   0.6263
   5.500   1.0649   0.00904   0.00339  -0.0969   0.4442   0.6287
   5.750   1.0929   0.00913   0.00351  -0.0972   0.4423   0.6316
   6.000   1.1208   0.00922   0.00364  -0.0975   0.4395   0.6348
   6.250   1.1493   0.00928   0.00375  -0.0978   0.4368   0.6379
   6.500   1.1774   0.00935   0.00386  -0.0981   0.4318   0.6411
   6.750   1.2042   0.00950   0.00399  -0.0983   0.4257   0.6441
   7.000   1.2323   0.00956   0.00411  -0.0986   0.4197   0.6473
   7.250   1.2586   0.00973   0.00427  -0.0987   0.4105   0.6510
   7.500   1.2859   0.00985   0.00443  -0.0989   0.4032   0.6549
   7.750   1.3119   0.01004   0.00463  -0.0989   0.3946   0.6588
   8.000   1.3374   0.01027   0.00485  -0.0988   0.3839   0.6623
   8.250   1.3609   0.01061   0.00516  -0.0985   0.3656   0.6664
   8.500   1.3785   0.01133   0.00572  -0.0973   0.3295   0.6706
   8.750   1.3830   0.01284   0.00687  -0.0942   0.2681   0.6745
   9.000   1.3615   0.01537   0.00888  -0.0873   0.1784   0.6782
   9.250   1.3309   0.01837   0.01153  -0.0803   0.1085   0.6828
   9.500   1.3121   0.02152   0.01453  -0.0768   0.0677   0.6879
   9.750   1.3095   0.02412   0.01709  -0.0756   0.0507   0.6927
  10.000   1.3120   0.02648   0.01949  -0.0750   0.0419   0.6978
  10.250   1.3156   0.02884   0.02189  -0.0746   0.0363   0.7035
  10.750   1.3207   0.03375   0.02690  -0.0737   0.0271   0.7153
  11.000   1.3204   0.03643   0.02962  -0.0731   0.0233   0.7224
  11.250   1.3224   0.03885   0.03209  -0.0725   0.0211   0.7294
  11.500   1.3233   0.04136   0.03465  -0.0718   0.0193   0.7373
  11.750   1.3245   0.04379   0.03715  -0.0712   0.0181   0.7450
  12.000   1.3267   0.04613   0.03957  -0.0706   0.0172   0.7538
  12.250   1.3285   0.04854   0.04205  -0.0700   0.0163   0.7635
  12.500   1.3299   0.05105   0.04464  -0.0695   0.0154   0.7752
  12.750   1.3327   0.05343   0.04712  -0.0690   0.0146   0.7919
  13.000   1.3364   0.05574   0.04959  -0.0687   0.0141   0.8244
  13.250   1.3389   0.05765   0.05183  -0.0678   0.0135   1.0002
  13.500   1.3421   0.06012   0.05434  -0.0674   0.0128   1.0002
  13.750   1.3455   0.06260   0.05685  -0.0672   0.0120   1.0002
  14.000   1.3482   0.06516   0.05945  -0.0669   0.0113   1.0002
  14.250   1.3526   0.06758   0.06191  -0.0667   0.0107   1.0002
  14.500   1.3572   0.06993   0.06430  -0.0665   0.0100   1.0002
  14.750   1.3599   0.07256   0.06697  -0.0664   0.0093   1.0002
  15.000   1.3632   0.07512   0.06956  -0.0662   0.0086   1.0002
  15.250   1.3674   0.07758   0.07206  -0.0661   0.0081   1.0002
  15.500   1.3703   0.08025   0.07476  -0.0661   0.0075   1.0002
  15.750   1.3738   0.08279   0.07734  -0.0660   0.0070   1.0002
  16.000   1.3766   0.08546   0.08004  -0.0660   0.0066   1.0002
  16.250   1.3792   0.08818   0.08281  -0.0661   0.0063   1.0002
  16.500   1.3830   0.09075   0.08542  -0.0661   0.0060   1.0002
  16.750   1.3856   0.09350   0.08822  -0.0662   0.0057   1.0002
  17.000   1.3879   0.09628   0.09104  -0.0664   0.0055   1.0002
  17.250   1.3909   0.09895   0.09376  -0.0665   0.0053   1.0002
  17.500   1.3924   0.10186   0.09672  -0.0667   0.0050   1.0002
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