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FX 66-S-196 AIRFOIL (fx66s196-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 66-S-196 AIRFOIL (fx66s196-il)
Reynolds number: 1,000,000
Max Cl/Cd: 130.83 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66s196-il-1000000-n5.txt
Download as CSV file: xf-fx66s196-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-S-196 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.6221   0.12126   0.11872  -0.0738   0.9113   0.0065
 -19.500  -0.6462   0.10977   0.10696  -0.0827   0.8869   0.0066
 -19.250  -0.6773   0.09964   0.09656  -0.0889   0.8642   0.0066
 -19.000  -0.6980   0.09212   0.08881  -0.0932   0.8416   0.0066
 -18.750  -0.7205   0.08473   0.08121  -0.0973   0.8228   0.0066
 -18.500  -0.7333   0.07908   0.07538  -0.1005   0.8066   0.0067
 -18.250  -0.7504   0.07302   0.06914  -0.1038   0.7936   0.0067
 -18.000  -0.7637   0.06773   0.06367  -0.1066   0.7792   0.0067
 -17.750  -0.7679   0.06390   0.05970  -0.1085   0.7652   0.0067
 -17.500  -0.7768   0.05963   0.05527  -0.1105   0.7549   0.0067
 -17.250  -0.7728   0.05707   0.05262  -0.1118   0.7442   0.0069
 -17.000  -0.7705   0.05438   0.04982  -0.1130   0.7349   0.0070
 -16.750  -0.7760   0.05095   0.04625  -0.1142   0.7259   0.0071
 -16.500  -0.7795   0.04794   0.04311  -0.1151   0.7182   0.0071
 -16.250  -0.7760   0.04574   0.04081  -0.1157   0.7108   0.0072
 -16.000  -0.7730   0.04357   0.03854  -0.1162   0.7044   0.0073
 -15.750  -0.7710   0.04141   0.03628  -0.1165   0.6985   0.0074
 -15.500  -0.7623   0.03991   0.03470  -0.1167   0.6925   0.0075
 -15.250  -0.7556   0.03827   0.03298  -0.1168   0.6877   0.0076
 -15.000  -0.7550   0.03621   0.03083  -0.1167   0.6824   0.0076
 -14.750  -0.7473   0.03483   0.02936  -0.1165   0.6768   0.0077
 -14.500  -0.7363   0.03368   0.02814  -0.1164   0.6718   0.0078
 -14.250  -0.7315   0.03213   0.02650  -0.1160   0.6663   0.0078
 -14.000  -0.7245   0.03078   0.02509  -0.1156   0.6610   0.0081
 -13.750  -0.7204   0.02924   0.02345  -0.1149   0.6567   0.0081
 -13.500  -0.7117   0.02805   0.02222  -0.1144   0.6520   0.0084
 -13.250  -0.7058   0.02672   0.02080  -0.1136   0.6475   0.0084
 -13.000  -0.6933   0.02584   0.01989  -0.1131   0.6435   0.0087
 -12.750  -0.6824   0.02486   0.01885  -0.1125   0.6398   0.0089
 -12.500  -0.6729   0.02381   0.01774  -0.1117   0.6361   0.0089
 -12.250  -0.6604   0.02298   0.01686  -0.1110   0.6322   0.0091
 -12.000  -0.6497   0.02205   0.01587  -0.1101   0.6287   0.0093
 -11.750  -0.6368   0.02124   0.01502  -0.1093   0.6254   0.0095
 -11.500  -0.6241   0.02046   0.01419  -0.1085   0.6216   0.0097
 -11.250  -0.6133   0.01960   0.01326  -0.1074   0.6175   0.0098
 -11.000  -0.6011   0.01886   0.01246  -0.1063   0.6140   0.0100
 -10.750  -0.5876   0.01821   0.01177  -0.1053   0.6111   0.0102
 -10.500  -0.5759   0.01752   0.01103  -0.1040   0.6079   0.0104
 -10.250  -0.5697   0.01679   0.01024  -0.1018   0.6045   0.0104
 -10.000  -0.5601   0.01636   0.00976  -0.0996   0.6013   0.0106
  -9.750  -0.5467   0.01580   0.00914  -0.0981   0.5983   0.0110
  -9.500  -0.5292   0.01533   0.00863  -0.0971   0.5958   0.0113
  -9.250  -0.5098   0.01492   0.00819  -0.0963   0.5931   0.0116
  -9.000  -0.4894   0.01454   0.00777  -0.0956   0.5904   0.0120
  -8.750  -0.4677   0.01421   0.00740  -0.0950   0.5877   0.0124
  -8.500  -0.4455   0.01389   0.00703  -0.0946   0.5851   0.0127
  -8.250  -0.4224   0.01360   0.00669  -0.0942   0.5828   0.0132
  -8.000  -0.3984   0.01331   0.00637  -0.0939   0.5809   0.0136
  -7.750  -0.3748   0.01298   0.00602  -0.0937   0.5789   0.0143
  -7.500  -0.3504   0.01269   0.00572  -0.0935   0.5769   0.0152
  -7.250  -0.3255   0.01243   0.00543  -0.0933   0.5748   0.0162
  -7.000  -0.3002   0.01220   0.00517  -0.0932   0.5725   0.0174
  -6.750  -0.2750   0.01196   0.00492  -0.0932   0.5700   0.0197
  -6.500  -0.2492   0.01177   0.00470  -0.0931   0.5672   0.0220
  -6.250  -0.2230   0.01153   0.00446  -0.0932   0.5654   0.0254
  -6.000  -0.1963   0.01133   0.00425  -0.0933   0.5635   0.0282
  -5.750  -0.1698   0.01111   0.00405  -0.0934   0.5616   0.0323
  -5.500  -0.1433   0.01089   0.00385  -0.0935   0.5598   0.0393
  -5.250  -0.1167   0.01067   0.00365  -0.0936   0.5580   0.0487
  -5.000  -0.0896   0.01051   0.00349  -0.0938   0.5563   0.0563
  -4.750  -0.0630   0.01029   0.00332  -0.0939   0.5546   0.0696
  -4.500  -0.0363   0.01008   0.00315  -0.0941   0.5529   0.0888
  -4.250  -0.0099   0.00982   0.00297  -0.0942   0.5513   0.1170
  -4.000   0.0165   0.00948   0.00278  -0.0944   0.5502   0.1552
  -3.750   0.0432   0.00919   0.00261  -0.0946   0.5490   0.1934
  -3.500   0.0675   0.00860   0.00234  -0.0946   0.5476   0.2841
  -3.250   0.0925   0.00812   0.00211  -0.0946   0.5462   0.3592
  -3.000   0.1183   0.00776   0.00194  -0.0947   0.5448   0.4261
  -2.750   0.1454   0.00760   0.00197  -0.0948   0.5434   0.4826
  -2.500   0.1746   0.00765   0.00196  -0.0952   0.5420   0.4973
  -2.250   0.2033   0.00766   0.00198  -0.0955   0.5406   0.5073
  -2.000   0.2322   0.00771   0.00197  -0.0959   0.5392   0.5138
  -1.750   0.2607   0.00772   0.00197  -0.0962   0.5379   0.5172
  -1.250   0.3182   0.00778   0.00199  -0.0968   0.5355   0.5249
  -1.000   0.3471   0.00780   0.00201  -0.0972   0.5344   0.5316
  -0.750   0.3759   0.00782   0.00204  -0.0976   0.5332   0.5355
  -0.500   0.4047   0.00784   0.00205  -0.0979   0.5320   0.5376
  -0.250   0.4335   0.00787   0.00207  -0.0983   0.5308   0.5393
   0.000   0.4623   0.00790   0.00208  -0.0987   0.5297   0.5403
   0.250   0.4909   0.00793   0.00210  -0.0990   0.5285   0.5413
   0.500   0.5195   0.00797   0.00212  -0.0994   0.5274   0.5421
   0.750   0.5480   0.00801   0.00214  -0.0997   0.5262   0.5430
   1.000   0.5764   0.00805   0.00217  -0.1000   0.5251   0.5435
   1.500   0.6328   0.00814   0.00225  -0.1006   0.5228   0.5442
   1.750   0.6608   0.00820   0.00230  -0.1008   0.5216   0.5447
   2.000   0.6891   0.00823   0.00235  -0.1012   0.5207   0.5452
   2.250   0.7175   0.00826   0.00240  -0.1015   0.5199   0.5457
   2.500   0.7458   0.00830   0.00246  -0.1018   0.5191   0.5462
   2.750   0.7740   0.00834   0.00252  -0.1021   0.5182   0.5469
   3.000   0.8021   0.00838   0.00258  -0.1024   0.5171   0.5476
   3.250   0.8301   0.00843   0.00266  -0.1027   0.5160   0.5484
   3.500   0.8580   0.00847   0.00273  -0.1030   0.5146   0.5491
   3.750   0.8856   0.00853   0.00280  -0.1032   0.5130   0.5498
   4.000   0.9131   0.00859   0.00288  -0.1034   0.5113   0.5504
   4.250   0.9402   0.00866   0.00296  -0.1035   0.5096   0.5510
   4.500   0.9672   0.00874   0.00306  -0.1036   0.5080   0.5517
   4.750   0.9940   0.00885   0.00317  -0.1037   0.5059   0.5524
   5.000   1.0215   0.00888   0.00326  -0.1039   0.5045   0.5533
   5.250   1.0488   0.00893   0.00335  -0.1041   0.5026   0.5544
   5.500   1.0758   0.00897   0.00345  -0.1042   0.5001   0.5556
   5.750   1.1025   0.00904   0.00355  -0.1043   0.4977   0.5566
   6.000   1.1286   0.00912   0.00365  -0.1042   0.4949   0.5576
   6.250   1.1533   0.00923   0.00377  -0.1039   0.4911   0.5585
   6.500   1.1798   0.00928   0.00388  -0.1039   0.4874   0.5593
   6.750   1.2050   0.00933   0.00397  -0.1037   0.4805   0.5605
   7.000   1.2285   0.00943   0.00409  -0.1032   0.4729   0.5619
   7.250   1.2507   0.00956   0.00423  -0.1025   0.4623   0.5633
   7.500   1.2705   0.00976   0.00441  -0.1012   0.4491   0.5648
   7.750   1.2825   0.01014   0.00471  -0.0986   0.4255   0.5664
   8.000   1.2779   0.01084   0.00522  -0.0929   0.3875   0.5680
   8.250   1.2693   0.01185   0.00604  -0.0868   0.3504   0.5697
   8.500   1.2590   0.01304   0.00708  -0.0810   0.3178   0.5714
   8.750   1.2452   0.01458   0.00847  -0.0754   0.2826   0.5729
   9.000   1.2409   0.01600   0.00980  -0.0716   0.2607   0.5746
   9.250   1.2267   0.01818   0.01185  -0.0673   0.2287   0.5764
   9.500   1.2100   0.02087   0.01439  -0.0634   0.1968   0.5785
   9.750   1.2082   0.02284   0.01633  -0.0613   0.1788   0.5808
  10.000   1.2005   0.02536   0.01876  -0.0590   0.1562   0.5830
  10.250   1.1931   0.02794   0.02127  -0.0569   0.1353   0.5853
  10.500   1.1874   0.03048   0.02374  -0.0551   0.1149   0.5876
  10.750   1.1821   0.03308   0.02626  -0.0535   0.0967   0.5895
  11.000   1.1812   0.03543   0.02857  -0.0523   0.0809   0.5920
  11.250   1.1823   0.03769   0.03080  -0.0514   0.0688   0.5945
  11.500   1.1844   0.03994   0.03303  -0.0506   0.0567   0.5978
  11.750   1.1884   0.04205   0.03512  -0.0499   0.0472   0.6010
  12.000   1.1926   0.04419   0.03725  -0.0493   0.0397   0.6039
  12.250   1.1986   0.04616   0.03922  -0.0488   0.0332   0.6070
  12.500   1.2033   0.04837   0.04142  -0.0484   0.0257   0.6106
  12.750   1.2098   0.05041   0.04346  -0.0481   0.0207   0.6145
  13.000   1.2186   0.05229   0.04539  -0.0480   0.0186   0.6195
  13.500   1.2366   0.05607   0.04925  -0.0479   0.0141   0.6307
  13.750   1.2444   0.05814   0.05136  -0.0479   0.0124   0.6375
  14.000   1.2540   0.06008   0.05335  -0.0480   0.0106   0.6449
  14.250   1.2623   0.06213   0.05545  -0.0481   0.0091   0.6533
  14.500   1.2716   0.06417   0.05756  -0.0484   0.0084   0.6615
  15.000   1.2909   0.06838   0.06190  -0.0492   0.0071   0.6839
  15.250   1.3009   0.07061   0.06422  -0.0498   0.0067   0.6974
  15.500   1.3121   0.07280   0.06650  -0.0506   0.0064   0.7135
  15.750   1.3222   0.07522   0.06901  -0.0517   0.0058   0.7311
  16.000   1.3371   0.07784   0.07177  -0.0537   0.0058   0.7601
  16.250   1.3510   0.08080   0.07489  -0.0562   0.0053   0.7915
  16.500   1.4133   0.08619   0.08076  -0.0704   0.0049   0.9436
  16.750   1.4143   0.08832   0.08294  -0.0690   0.0048   0.9983
  17.000   1.4258   0.09137   0.08604  -0.0708   0.0046   0.9999
  17.250   1.4319   0.09392   0.08864  -0.0712   0.0044   1.0000
  17.500   1.4356   0.09660   0.09137  -0.0714   0.0043   1.0000
  17.750   1.4387   0.09935   0.09416  -0.0715   0.0041   1.0000
  18.000   1.4414   0.10215   0.09701  -0.0717   0.0040   1.0000
  18.250   1.4424   0.10524   0.10017  -0.0720   0.0038   1.0000
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