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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=9


Details Polar file
Airfoil: WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA) (fx6617ai-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.86 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx6617ai-il-1000000.txt
Download as CSV file: xf-fx6617ai-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7108   0.09465   0.09253  -0.0465   0.9998   0.0105
 -16.000  -0.7360   0.08538   0.08311  -0.0523   0.9998   0.0105
 -15.750  -0.7593   0.07705   0.07462  -0.0575   0.9998   0.0104
 -15.500  -0.7801   0.06975   0.06716  -0.0620   0.9998   0.0104
 -15.250  -0.8010   0.06296   0.06020  -0.0660   0.9998   0.0105
 -15.000  -0.8178   0.05712   0.05378  -0.0698   0.8384   0.0106
 -14.750  -0.8313   0.05277   0.04905  -0.0716   0.7767   0.0106
 -14.500  -0.8396   0.04899   0.04500  -0.0732   0.7396   0.0107
 -14.250  -0.8430   0.04587   0.04168  -0.0745   0.7115   0.0108
 -14.000  -0.8430   0.04316   0.03880  -0.0756   0.6892   0.0109
 -13.500  -0.8358   0.03864   0.03401  -0.0773   0.6589   0.0112
 -13.250  -0.8300   0.03664   0.03188  -0.0781   0.6483   0.0113
 -13.000  -0.8229   0.03479   0.02991  -0.0787   0.6391   0.0114
 -12.750  -0.8148   0.03302   0.02803  -0.0793   0.6312   0.0116
 -12.500  -0.8054   0.03139   0.02627  -0.0798   0.6240   0.0118
 -12.250  -0.7947   0.02985   0.02463  -0.0801   0.6180   0.0120
 -12.000  -0.7827   0.02844   0.02309  -0.0805   0.6122   0.0123
 -11.750  -0.7694   0.02710   0.02163  -0.0808   0.6072   0.0125
 -11.500  -0.7547   0.02586   0.02030  -0.0812   0.6029   0.0128
 -11.250  -0.7407   0.02488   0.01919  -0.0812   0.5986   0.0130
 -11.000  -0.7234   0.02415   0.01835  -0.0809   0.5943   0.0132
 -10.750  -0.7030   0.02358   0.01768  -0.0810   0.5908   0.0134
 -10.500  -0.6908   0.02149   0.01544  -0.0801   0.5878   0.0139
 -10.250  -0.6714   0.02056   0.01446  -0.0799   0.5845   0.0143
 -10.000  -0.6492   0.02000   0.01385  -0.0799   0.5810   0.0147
  -9.750  -0.6262   0.01951   0.01330  -0.0799   0.5771   0.0150
  -9.500  -0.6025   0.01897   0.01272  -0.0800   0.5747   0.0154
  -9.250  -0.5788   0.01841   0.01210  -0.0800   0.5719   0.0158
  -9.000  -0.5551   0.01782   0.01146  -0.0799   0.5690   0.0161
  -8.750  -0.5311   0.01726   0.01083  -0.0798   0.5663   0.0164
  -8.500  -0.5070   0.01674   0.01023  -0.0798   0.5634   0.0166
  -8.250  -0.4823   0.01625   0.00967  -0.0798   0.5607   0.0169
  -8.000  -0.4570   0.01577   0.00915  -0.0798   0.5588   0.0170
  -7.750  -0.4314   0.01533   0.00866  -0.0799   0.5566   0.0172
  -7.500  -0.4081   0.01454   0.00781  -0.0798   0.5544   0.0176
  -7.250  -0.3841   0.01385   0.00706  -0.0797   0.5520   0.0183
  -7.000  -0.3580   0.01348   0.00665  -0.0798   0.5495   0.0190
  -6.750  -0.3317   0.01315   0.00625  -0.0799   0.5466   0.0195
  -6.500  -0.3048   0.01281   0.00587  -0.0801   0.5446   0.0201
  -6.250  -0.2776   0.01248   0.00551  -0.0803   0.5430   0.0207
  -6.000  -0.2500   0.01220   0.00520  -0.0805   0.5411   0.0215
  -5.750  -0.2225   0.01191   0.00486  -0.0807   0.5391   0.0222
  -5.500  -0.1954   0.01154   0.00446  -0.0808   0.5372   0.0243
  -5.250  -0.1676   0.01133   0.00422  -0.0811   0.5352   0.0264
  -5.000  -0.1399   0.01110   0.00396  -0.0813   0.5331   0.0298
  -4.750  -0.1123   0.01092   0.00375  -0.0815   0.5304   0.0357
  -4.500  -0.0847   0.01057   0.00348  -0.0817   0.5289   0.0521
  -4.250  -0.0584   0.01000   0.00317  -0.0820   0.5274   0.1130
  -4.000  -0.0324   0.00939   0.00287  -0.0822   0.5257   0.1946
  -3.750  -0.0063   0.00879   0.00260  -0.0825   0.5240   0.2839
  -3.500   0.0196   0.00819   0.00237  -0.0827   0.5223   0.3906
  -3.250   0.0477   0.00798   0.00229  -0.0830   0.5206   0.4412
  -3.000   0.0762   0.00788   0.00224  -0.0833   0.5189   0.4720
  -2.750   0.1048   0.00784   0.00224  -0.0836   0.5169   0.4966
  -2.500   0.1337   0.00787   0.00227  -0.0839   0.5146   0.5179
  -2.250   0.1631   0.00785   0.00226  -0.0843   0.5134   0.5303
  -2.000   0.1925   0.00785   0.00228  -0.0847   0.5119   0.5438
  -1.750   0.2219   0.00787   0.00231  -0.0850   0.5104   0.5568
  -1.500   0.2515   0.00792   0.00232  -0.0855   0.5088   0.5643
  -1.250   0.2809   0.00792   0.00232  -0.0859   0.5072   0.5695
  -1.000   0.3103   0.00796   0.00234  -0.0863   0.5057   0.5752
  -0.750   0.3398   0.00802   0.00235  -0.0867   0.5041   0.5805
  -0.500   0.3689   0.00806   0.00238  -0.0871   0.5024   0.5858
  -0.250   0.3980   0.00816   0.00245  -0.0874   0.5003   0.5908
   0.000   0.4274   0.00822   0.00249  -0.0879   0.4988   0.5951
   0.250   0.4570   0.00823   0.00250  -0.0883   0.4976   0.5985
   0.500   0.4863   0.00824   0.00252  -0.0888   0.4963   0.6022
   0.750   0.5156   0.00827   0.00256  -0.0892   0.4949   0.6059
   1.000   0.5450   0.00832   0.00260  -0.0896   0.4934   0.6094
   1.250   0.5744   0.00837   0.00263  -0.0901   0.4920   0.6125
   1.500   0.6036   0.00839   0.00266  -0.0905   0.4905   0.6158
   1.750   0.6326   0.00843   0.00270  -0.0909   0.4890   0.6191
   2.000   0.6616   0.00851   0.00277  -0.0913   0.4872   0.6224
   2.250   0.6905   0.00864   0.00287  -0.0917   0.4851   0.6258
   2.500   0.7197   0.00871   0.00295  -0.0922   0.4839   0.6287
   2.750   0.7488   0.00872   0.00300  -0.0926   0.4828   0.6319
   3.000   0.7779   0.00875   0.00307  -0.0930   0.4816   0.6349
   3.250   0.8069   0.00880   0.00314  -0.0934   0.4802   0.6381
   3.500   0.8359   0.00886   0.00322  -0.0939   0.4787   0.6413
   3.750   0.8649   0.00892   0.00328  -0.0943   0.4771   0.6443
   4.000   0.8937   0.00896   0.00335  -0.0947   0.4756   0.6474
   4.250   0.9224   0.00902   0.00344  -0.0951   0.4742   0.6505
   4.500   0.9510   0.00911   0.00355  -0.0955   0.4727   0.6536
   4.750   0.9795   0.00925   0.00369  -0.0958   0.4707   0.6568
   5.000   1.0082   0.00937   0.00382  -0.0962   0.4691   0.6600
   5.250   1.0368   0.00940   0.00392  -0.0966   0.4680   0.6632
   5.500   1.0653   0.00945   0.00403  -0.0970   0.4667   0.6664
   5.750   1.0937   0.00951   0.00414  -0.0974   0.4649   0.6698
   6.000   1.1221   0.00954   0.00421  -0.0977   0.4625   0.6734
   6.250   1.1504   0.00960   0.00429  -0.0980   0.4601   0.6767
   6.500   1.1778   0.00968   0.00439  -0.0983   0.4561   0.6804
   6.750   1.2057   0.00970   0.00448  -0.0985   0.4525   0.6842
   7.000   1.2338   0.00970   0.00454  -0.0988   0.4486   0.6883
   7.250   1.2613   0.00975   0.00460  -0.0990   0.4435   0.6923
   7.500   1.2882   0.00986   0.00475  -0.0992   0.4395   0.6967
   7.750   1.3162   0.00989   0.00487  -0.0995   0.4359   0.7015
   8.000   1.3437   0.00996   0.00499  -0.0997   0.4314   0.7064
   8.250   1.3697   0.01011   0.00515  -0.0997   0.4255   0.7113
   8.500   1.3972   0.01015   0.00529  -0.1000   0.4182   0.7167
   8.750   1.4227   0.01032   0.00545  -0.0999   0.4064   0.7225
   9.000   1.4459   0.01061   0.00570  -0.0995   0.3860   0.7281
   9.250   1.4621   0.01134   0.00626  -0.0981   0.3456   0.7348
   9.500   1.4592   0.01318   0.00766  -0.0939   0.2716   0.7419
   9.750   1.4389   0.01547   0.00956  -0.0872   0.1998   0.7502
  10.000   1.4157   0.01811   0.01195  -0.0813   0.1473   0.7597
  10.250   1.3987   0.02108   0.01481  -0.0778   0.1124   0.7711
  10.500   1.3815   0.02490   0.01857  -0.0760   0.0821   0.7851
  10.750   1.3692   0.02872   0.02241  -0.0750   0.0616   0.8045
  11.000   1.3618   0.03193   0.02579  -0.0740   0.0501   0.8591
  11.250   1.3561   0.03472   0.02879  -0.0728   0.0431   1.0002
  11.500   1.3518   0.03779   0.03188  -0.0721   0.0376   1.0002
  11.750   1.3509   0.04049   0.03462  -0.0714   0.0337   1.0002
  12.000   1.3468   0.04346   0.03760  -0.0706   0.0298   1.0002
  12.250   1.3466   0.04605   0.04023  -0.0699   0.0275   1.0002
  12.500   1.3453   0.04880   0.04300  -0.0692   0.0251   1.0002
  12.750   1.3444   0.05158   0.04582  -0.0687   0.0231   1.0002
  13.000   1.3470   0.05405   0.04834  -0.0683   0.0219   1.0002
  13.250   1.3482   0.05672   0.05103  -0.0679   0.0206   1.0002
  13.500   1.3485   0.05948   0.05382  -0.0675   0.0192   1.0002
  13.750   1.3503   0.06212   0.05650  -0.0672   0.0181   1.0002
  14.000   1.3542   0.06454   0.05897  -0.0669   0.0172   1.0002
  14.250   1.3560   0.06725   0.06172  -0.0667   0.0163   1.0002
  14.500   1.3572   0.06999   0.06449  -0.0664   0.0152   1.0002
  14.750   1.3570   0.07295   0.06750  -0.0662   0.0143   1.0002
  15.000   1.3622   0.07530   0.06990  -0.0661   0.0136   1.0002
  15.250   1.3656   0.07787   0.07251  -0.0660   0.0129   1.0002
  15.500   1.3674   0.08065   0.07533  -0.0659   0.0122   1.0002
  15.750   1.3668   0.08368   0.07839  -0.0658   0.0113   1.0002
  16.000   1.3701   0.08633   0.08110  -0.0658   0.0109   1.0002
  16.250   1.3743   0.08886   0.08367  -0.0659   0.0104   1.0002
  16.500   1.3787   0.09137   0.08622  -0.0659   0.0098   1.0002
  16.750   1.3804   0.09424   0.08913  -0.0661   0.0092   1.0002
  17.000   1.3800   0.09737   0.09229  -0.0662   0.0087   1.0002
  17.250   1.3834   0.10001   0.09499  -0.0664   0.0083   1.0002
  17.500   1.3858   0.10284   0.09787  -0.0666   0.0079   1.0002
  17.750   1.3890   0.10555   0.10063  -0.0669   0.0075   1.0002
  18.000   1.3913   0.10838   0.10349  -0.0672   0.0071   1.0002
  18.250   1.3888   0.11191   0.10706  -0.0677   0.0066   1.0002
  18.500   1.3887   0.11508   0.11029  -0.0682   0.0063   1.0002
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