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SG6040 (sg6040-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SG6040 (sg6040-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.26 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6040-il-1000000-n5.txt
Download as CSV file: xf-sg6040-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6040                                          
  
 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  -0.8063   0.11003   0.10719  -0.0558   1.0000   0.0080
 -18.250  -0.8277   0.10250   0.09956  -0.0595   1.0000   0.0080
 -18.000  -0.8507   0.09480   0.09174  -0.0634   1.0000   0.0080
 -17.750  -0.8732   0.08734   0.08417  -0.0672   1.0000   0.0080
 -17.500  -0.8911   0.08077   0.07749  -0.0705   1.0000   0.0080
 -17.250  -0.9126   0.07380   0.07039  -0.0740   1.0000   0.0080
 -17.000  -0.9278   0.06803   0.06451  -0.0769   1.0000   0.0080
 -16.750  -0.9409   0.06277   0.05914  -0.0794   1.0000   0.0080
 -16.500  -0.9527   0.05800   0.05425  -0.0815   1.0000   0.0081
 -16.250  -0.9624   0.05378   0.04994  -0.0831   1.0000   0.0081
 -16.000  -0.9707   0.05001   0.04607  -0.0843   1.0000   0.0081
 -15.750  -0.9772   0.04676   0.04273  -0.0850   1.0000   0.0081
 -15.500  -0.9839   0.04373   0.03961  -0.0853   1.0000   0.0082
 -15.250  -0.9863   0.04130   0.03711  -0.0852   1.0000   0.0082
 -15.000  -0.9910   0.03880   0.03452  -0.0849   1.0000   0.0082
 -14.750  -0.9925   0.03674   0.03240  -0.0842   1.0000   0.0083
 -14.500  -0.9967   0.03459   0.03017  -0.0833   1.0000   0.0083
 -14.250  -0.9922   0.03282   0.02833  -0.0831   0.9997   0.0084
 -14.000  -0.9764   0.03086   0.02630  -0.0852   0.9985   0.0085
 -13.750  -0.9602   0.02898   0.02433  -0.0873   0.9966   0.0086
 -13.500  -0.9421   0.02732   0.02260  -0.0892   0.9945   0.0087
 -13.250  -0.9248   0.02585   0.02105  -0.0905   0.9919   0.0088
 -13.000  -0.9071   0.02445   0.01958  -0.0918   0.9887   0.0088
 -12.750  -0.8854   0.02324   0.01830  -0.0934   0.9858   0.0089
 -12.250  -0.8459   0.02098   0.01592  -0.0954   0.9773   0.0090
 -12.000  -0.8229   0.02004   0.01491  -0.0965   0.9726   0.0091
 -11.750  -0.8025   0.01919   0.01401  -0.0970   0.9653   0.0092
 -11.250  -0.7500   0.01717   0.01185  -0.1004   0.9490   0.0096
 -11.000  -0.7200   0.01636   0.01097  -0.1022   0.9390   0.0097
 -10.750  -0.6912   0.01569   0.01023  -0.1036   0.9262   0.0100
 -10.500  -0.6662   0.01518   0.00963  -0.1039   0.9112   0.0101
 -10.250  -0.6453   0.01476   0.00913  -0.1033   0.8963   0.0104
 -10.000  -0.6257   0.01438   0.00866  -0.1022   0.8828   0.0106
  -9.750  -0.6059   0.01401   0.00822  -0.1012   0.8712   0.0108
  -9.500  -0.5854   0.01368   0.00781  -0.1003   0.8605   0.0110
  -9.250  -0.5643   0.01336   0.00743  -0.0994   0.8506   0.0112
  -9.000  -0.5427   0.01306   0.00706  -0.0986   0.8417   0.0114
  -8.750  -0.5206   0.01275   0.00669  -0.0978   0.8328   0.0116
  -8.500  -0.4980   0.01246   0.00635  -0.0971   0.8250   0.0118
  -8.250  -0.4756   0.01213   0.00596  -0.0964   0.8166   0.0123
  -8.000  -0.4523   0.01186   0.00565  -0.0958   0.8092   0.0127
  -7.750  -0.4283   0.01159   0.00535  -0.0953   0.8016   0.0131
  -7.250  -0.3793   0.01114   0.00480  -0.0944   0.7871   0.0143
  -7.000  -0.3548   0.01089   0.00453  -0.0940   0.7799   0.0155
  -6.750  -0.3298   0.01067   0.00428  -0.0936   0.7731   0.0173
  -6.500  -0.3049   0.01041   0.00402  -0.0933   0.7660   0.0214
  -6.250  -0.2807   0.01011   0.00374  -0.0928   0.7592   0.0317
  -6.000  -0.2558   0.00979   0.00348  -0.0925   0.7523   0.0451
  -5.750  -0.2307   0.00954   0.00327  -0.0922   0.7450   0.0589
  -5.500  -0.2046   0.00934   0.00310  -0.0921   0.7385   0.0691
  -5.250  -0.1782   0.00919   0.00294  -0.0919   0.7306   0.0765
  -5.000  -0.1518   0.00905   0.00280  -0.0918   0.7234   0.0852
  -4.750  -0.1251   0.00889   0.00265  -0.0917   0.7156   0.0945
  -4.500  -0.0989   0.00873   0.00251  -0.0915   0.7079   0.1074
  -4.250  -0.0723   0.00855   0.00238  -0.0914   0.7000   0.1245
  -4.000  -0.0465   0.00834   0.00223  -0.0912   0.6921   0.1505
  -3.750  -0.0197   0.00813   0.00210  -0.0912   0.6848   0.1761
  -3.500   0.0065   0.00795   0.00198  -0.0910   0.6767   0.2055
  -3.250   0.0331   0.00770   0.00185  -0.0910   0.6696   0.2443
  -3.000   0.0593   0.00746   0.00173  -0.0909   0.6614   0.2887
  -2.750   0.0861   0.00723   0.00161  -0.0909   0.6543   0.3315
  -2.500   0.1129   0.00702   0.00152  -0.0909   0.6465   0.3753
  -2.250   0.1397   0.00683   0.00144  -0.0908   0.6392   0.4223
  -2.000   0.1668   0.00666   0.00139  -0.0908   0.6311   0.4672
  -1.750   0.1942   0.00660   0.00137  -0.0908   0.6238   0.4949
  -1.500   0.2222   0.00658   0.00137  -0.0909   0.6160   0.5138
  -1.250   0.2498   0.00660   0.00138  -0.0908   0.6082   0.5299
  -1.000   0.2780   0.00661   0.00140  -0.0909   0.6006   0.5450
  -0.500   0.3336   0.00669   0.00145  -0.0909   0.5843   0.5693
   0.000   0.3891   0.00678   0.00151  -0.0909   0.5684   0.5848
   0.250   0.4167   0.00685   0.00154  -0.0908   0.5603   0.5909
   0.500   0.4446   0.00689   0.00158  -0.0908   0.5533   0.5963
   0.750   0.4722   0.00695   0.00161  -0.0908   0.5453   0.6004
   1.000   0.4999   0.00702   0.00165  -0.0908   0.5378   0.6035
   1.500   0.5549   0.00715   0.00174  -0.0907   0.5228   0.6093
   1.750   0.5823   0.00722   0.00180  -0.0906   0.5145   0.6124
   2.000   0.6094   0.00730   0.00186  -0.0905   0.5069   0.6155
   2.250   0.6369   0.00737   0.00192  -0.0904   0.4995   0.6184
   2.500   0.6636   0.00748   0.00199  -0.0903   0.4916   0.6213
   2.750   0.6908   0.00756   0.00206  -0.0902   0.4832   0.6238
   3.000   0.7170   0.00767   0.00215  -0.0899   0.4731   0.6266
   3.500   0.7686   0.00794   0.00235  -0.0892   0.4466   0.6331
   3.750   0.7942   0.00808   0.00246  -0.0888   0.4335   0.6362
   4.000   0.8196   0.00824   0.00257  -0.0884   0.4218   0.6391
   4.250   0.8441   0.00843   0.00271  -0.0879   0.4051   0.6421
   4.500   0.8684   0.00862   0.00285  -0.0873   0.3898   0.6457
   4.750   0.8928   0.00880   0.00300  -0.0867   0.3770   0.6492
   5.000   0.9173   0.00898   0.00315  -0.0861   0.3639   0.6527
   5.250   0.9408   0.00920   0.00332  -0.0854   0.3482   0.6563
   5.500   0.9629   0.00947   0.00352  -0.0845   0.3291   0.6599
   5.750   0.9838   0.00979   0.00376  -0.0833   0.3044   0.6641
   6.000   1.0034   0.01016   0.00402  -0.0819   0.2804   0.6684
   6.250   1.0230   0.01052   0.00429  -0.0805   0.2568   0.6726
   6.750   1.0550   0.01133   0.00489  -0.0764   0.2082   0.6812
   7.000   1.0697   0.01178   0.00525  -0.0741   0.1862   0.6864
   7.250   1.0854   0.01222   0.00561  -0.0721   0.1669   0.6920
   7.500   1.1007   0.01266   0.00600  -0.0700   0.1496   0.6975
   7.750   1.1157   0.01313   0.00640  -0.0679   0.1331   0.7038
   8.000   1.1318   0.01356   0.00679  -0.0660   0.1207   0.7098
   8.250   1.1475   0.01399   0.00720  -0.0642   0.1090   0.7161
   8.500   1.1625   0.01447   0.00765  -0.0622   0.0979   0.7234
   8.750   1.1777   0.01493   0.00810  -0.0603   0.0891   0.7304
   9.000   1.1925   0.01542   0.00858  -0.0584   0.0814   0.7388
   9.250   1.2074   0.01591   0.00908  -0.0566   0.0737   0.7472
   9.500   1.2212   0.01645   0.00962  -0.0547   0.0671   0.7573
   9.750   1.2350   0.01700   0.01019  -0.0528   0.0613   0.7683
  10.000   1.2490   0.01756   0.01078  -0.0510   0.0563   0.7812
  10.250   1.2615   0.01819   0.01144  -0.0491   0.0518   0.7963
  10.500   1.2748   0.01878   0.01210  -0.0474   0.0482   0.8135
  10.750   1.2867   0.01943   0.01281  -0.0454   0.0449   0.8350
  11.000   1.2979   0.02005   0.01355  -0.0434   0.0424   0.8679
  11.500   1.3247   0.02144   0.01516  -0.0407   0.0376   1.0000
  11.750   1.3376   0.02227   0.01601  -0.0393   0.0361   1.0000
  12.000   1.3501   0.02314   0.01691  -0.0380   0.0345   1.0000
  12.250   1.3614   0.02413   0.01791  -0.0366   0.0328   1.0000
  12.500   1.3716   0.02521   0.01901  -0.0352   0.0312   1.0000
  12.750   1.3834   0.02622   0.02006  -0.0341   0.0300   1.0000
  13.000   1.3941   0.02733   0.02120  -0.0329   0.0288   1.0000
  13.250   1.4037   0.02855   0.02245  -0.0317   0.0277   1.0000
  13.500   1.4123   0.02989   0.02383  -0.0306   0.0266   1.0000
  13.750   1.4220   0.03118   0.02516  -0.0296   0.0258   1.0000
  14.000   1.4314   0.03253   0.02656  -0.0287   0.0250   1.0000
  14.250   1.4397   0.03400   0.02807  -0.0278   0.0242   1.0000
  14.500   1.4472   0.03560   0.02971  -0.0269   0.0234   1.0000
  14.750   1.4539   0.03731   0.03146  -0.0261   0.0227   1.0000
  15.000   1.4602   0.03910   0.03330  -0.0254   0.0220   1.0000
  15.250   1.4676   0.04085   0.03511  -0.0249   0.0215   1.0000
  15.500   1.4739   0.04275   0.03707  -0.0244   0.0210   1.0000
  15.750   1.4796   0.04475   0.03913  -0.0240   0.0204   1.0000
  16.000   1.4846   0.04688   0.04131  -0.0237   0.0199   1.0000
  16.250   1.4886   0.04916   0.04364  -0.0234   0.0193   1.0000
  16.500   1.4915   0.05163   0.04616  -0.0233   0.0188   1.0000
  16.750   1.4941   0.05420   0.04880  -0.0233   0.0184   1.0000
  17.000   1.4982   0.05665   0.05133  -0.0234   0.0180   1.0000
  17.250   1.5014   0.05926   0.05400  -0.0235   0.0177   1.0000
  17.500   1.5035   0.06204   0.05685  -0.0238   0.0174   1.0000
  17.750   1.5050   0.06497   0.05985  -0.0243   0.0170   1.0000
  18.000   1.5056   0.06807   0.06303  -0.0248   0.0167   1.0000
  18.250   1.5060   0.07126   0.06629  -0.0254   0.0164   1.0000
  18.500   1.5052   0.07465   0.06975  -0.0262   0.0161   1.0000
  18.750   1.5035   0.07825   0.07343  -0.0271   0.0159   1.0000
  19.000   1.5003   0.08212   0.07738  -0.0283   0.0156   1.0000
  19.250   1.4959   0.08626   0.08160  -0.0296   0.0153   1.0000
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