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NACA M6 AIRFOIL (m6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA M6 AIRFOIL (m6-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.65 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-m6-il-1000000-n5.txt
Download as CSV file: xf-m6-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA M6 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.2580   0.04553   0.04266  -0.0404   1.0000   0.0171
 -15.500  -1.2666   0.04221   0.03922  -0.0404   1.0000   0.0172
 -15.250  -1.2710   0.03967   0.03657  -0.0394   1.0000   0.0173
 -15.000  -1.2691   0.03790   0.03470  -0.0381   1.0000   0.0174
 -14.750  -1.2629   0.03661   0.03334  -0.0366   1.0000   0.0175
 -14.500  -1.2556   0.03547   0.03214  -0.0349   1.0000   0.0176
 -14.250  -1.2479   0.03442   0.03102  -0.0330   1.0000   0.0177
 -14.000  -1.2404   0.03339   0.02992  -0.0309   1.0000   0.0178
 -13.750  -1.2320   0.03248   0.02893  -0.0286   1.0000   0.0179
 -13.500  -1.2221   0.03162   0.02801  -0.0264   1.0000   0.0181
 -13.250  -1.2074   0.03089   0.02721  -0.0249   1.0000   0.0182
 -13.000  -1.1926   0.03005   0.02628  -0.0235   1.0000   0.0184
 -12.750  -1.1772   0.02917   0.02531  -0.0220   1.0000   0.0186
 -12.500  -1.1617   0.02819   0.02424  -0.0206   1.0000   0.0188
 -12.250  -1.1453   0.02723   0.02317  -0.0193   1.0000   0.0190
 -12.000  -1.1276   0.02634   0.02218  -0.0181   1.0000   0.0192
 -11.750  -1.1091   0.02548   0.02120  -0.0170   1.0000   0.0195
 -11.500  -1.0903   0.02456   0.02017  -0.0159   1.0000   0.0197
 -11.250  -1.0710   0.02365   0.01914  -0.0149   1.0000   0.0199
 -11.000  -1.0507   0.02280   0.01818  -0.0139   1.0000   0.0201
 -10.750  -1.0293   0.02207   0.01735  -0.0131   1.0000   0.0202
 -10.500  -1.0068   0.02146   0.01665  -0.0124   1.0000   0.0204
 -10.250  -0.9791   0.02088   0.01597  -0.0128   0.9597   0.0205
 -10.000  -0.9584   0.02036   0.01530  -0.0115   0.9289   0.0206
  -9.750  -0.9389   0.01959   0.01437  -0.0101   0.9074   0.0208
  -9.500  -0.9196   0.01853   0.01315  -0.0087   0.8900   0.0211
  -9.250  -0.8975   0.01786   0.01237  -0.0078   0.8741   0.0213
  -9.000  -0.8743   0.01732   0.01173  -0.0071   0.8589   0.0214
  -8.750  -0.8503   0.01686   0.01117  -0.0064   0.8440   0.0216
  -8.500  -0.8257   0.01646   0.01069  -0.0059   0.8288   0.0218
  -8.250  -0.8007   0.01610   0.01024  -0.0054   0.8133   0.0220
  -8.000  -0.7755   0.01571   0.00976  -0.0049   0.7979   0.0223
  -7.500  -0.7248   0.01488   0.00874  -0.0041   0.7685   0.0226
  -7.250  -0.6990   0.01449   0.00826  -0.0037   0.7552   0.0228
  -7.000  -0.6732   0.01411   0.00779  -0.0034   0.7426   0.0230
  -6.750  -0.6471   0.01374   0.00734  -0.0031   0.7309   0.0232
  -6.500  -0.6209   0.01339   0.00691  -0.0028   0.7196   0.0234
  -6.250  -0.5945   0.01305   0.00651  -0.0025   0.7096   0.0236
  -5.750  -0.5413   0.01243   0.00575  -0.0020   0.6904   0.0241
  -5.500  -0.5145   0.01215   0.00541  -0.0018   0.6817   0.0243
  -5.250  -0.4875   0.01188   0.00509  -0.0016   0.6731   0.0245
  -5.000  -0.4603   0.01166   0.00482  -0.0015   0.6650   0.0247
  -4.750  -0.4329   0.01145   0.00457  -0.0014   0.6569   0.0250
  -4.500  -0.4054   0.01127   0.00434  -0.0013   0.6492   0.0251
  -4.250  -0.3784   0.01098   0.00401  -0.0011   0.6418   0.0254
  -3.750  -0.3242   0.01043   0.00339  -0.0007   0.6273   0.0262
  -3.500  -0.2966   0.01024   0.00316  -0.0007   0.6200   0.0266
  -3.250  -0.2689   0.01007   0.00297  -0.0006   0.6134   0.0270
  -3.000  -0.2410   0.00991   0.00279  -0.0006   0.6062   0.0274
  -2.750  -0.2132   0.00977   0.00262  -0.0006   0.5997   0.0278
  -2.500  -0.1851   0.00964   0.00247  -0.0006   0.5928   0.0283
  -2.250  -0.1571   0.00953   0.00233  -0.0006   0.5859   0.0288
  -2.000  -0.1289   0.00941   0.00220  -0.0006   0.5796   0.0293
  -1.750  -0.1007   0.00931   0.00208  -0.0006   0.5724   0.0298
  -1.500  -0.0724   0.00923   0.00198  -0.0007   0.5660   0.0303
  -1.250  -0.0441   0.00914   0.00187  -0.0007   0.5591   0.0314
  -1.000  -0.0160   0.00906   0.00178  -0.0008   0.5521   0.0334
  -0.750   0.0124   0.00897   0.00170  -0.0009   0.5456   0.0355
  -0.500   0.0406   0.00889   0.00163  -0.0009   0.5382   0.0414
  -0.250   0.0682   0.00870   0.00156  -0.0009   0.5316   0.0754
   0.000   0.0961   0.00859   0.00152  -0.0009   0.5241   0.0999
   0.250   0.1238   0.00844   0.00148  -0.0009   0.5172   0.1386
   0.500   0.1517   0.00832   0.00146  -0.0010   0.5096   0.1714
   0.750   0.1792   0.00816   0.00143  -0.0010   0.5022   0.2240
   1.000   0.2054   0.00784   0.00141  -0.0009   0.4944   0.3280
   1.250   0.2163   0.00615   0.00128   0.0022   0.4877   0.7953
   1.500   0.2405   0.00598   0.00137   0.0033   0.4797   0.8757
   1.750   0.2673   0.00601   0.00145   0.0037   0.4707   0.9078
   2.000   0.2948   0.00610   0.00153   0.0040   0.4595   0.9264
   2.250   0.3224   0.00621   0.00162   0.0042   0.4471   0.9401
   2.500   0.3499   0.00634   0.00173   0.0044   0.4371   0.9533
   2.750   0.3779   0.00646   0.00183   0.0045   0.4286   0.9613
   3.000   0.4079   0.00656   0.00190   0.0041   0.4209   0.9643
   3.250   0.4370   0.00670   0.00198   0.0038   0.4090   0.9681
   3.500   0.4639   0.00682   0.00206   0.0040   0.3953   0.9720
   3.750   0.4949   0.00693   0.00213   0.0033   0.3858   0.9731
   4.000   0.5257   0.00705   0.00222   0.0025   0.3764   0.9742
   4.250   0.5565   0.00719   0.00232   0.0018   0.3642   0.9754
   4.500   0.5867   0.00738   0.00243   0.0011   0.3456   0.9767
   4.750   0.6162   0.00762   0.00257   0.0005   0.3202   0.9782
   5.000   0.6453   0.00787   0.00272   0.0000   0.2988   0.9799
   5.250   0.6736   0.00808   0.00287  -0.0003   0.2817   0.9818
   5.500   0.7008   0.00839   0.00306  -0.0004   0.2556   0.9837
   5.750   0.7311   0.00874   0.00328  -0.0013   0.2277   0.9843
   6.000   0.7614   0.00911   0.00352  -0.0023   0.2018   0.9850
   6.250   0.7914   0.00950   0.00379  -0.0031   0.1775   0.9857
   6.500   0.8214   0.00982   0.00404  -0.0040   0.1589   0.9865
   6.750   0.8504   0.01023   0.00433  -0.0047   0.1368   0.9875
   7.000   0.8776   0.01084   0.00475  -0.0052   0.0991   0.9887
   7.250   0.9053   0.01131   0.00512  -0.0057   0.0806   0.9899
   7.500   0.9333   0.01169   0.00545  -0.0061   0.0699   0.9913
   7.750   0.9605   0.01209   0.00579  -0.0064   0.0592   0.9928
   8.000   0.9875   0.01250   0.00615  -0.0068   0.0487   0.9940
   8.250   1.0161   0.01291   0.00651  -0.0074   0.0413   0.9946
   8.500   1.0444   0.01331   0.00689  -0.0080   0.0366   0.9954
   8.750   1.0728   0.01366   0.00724  -0.0087   0.0340   0.9963
   9.000   1.1009   0.01405   0.00763  -0.0092   0.0316   0.9972
   9.250   1.1285   0.01446   0.00804  -0.0098   0.0294   0.9983
   9.500   1.1562   0.01482   0.00843  -0.0103   0.0281   0.9992
   9.750   1.1831   0.01524   0.00886  -0.0107   0.0265   1.0000
  10.000   1.2001   0.01564   0.00927  -0.0090   0.0250   1.0000
  10.250   1.2169   0.01601   0.00966  -0.0072   0.0239   1.0000
  10.500   1.2336   0.01637   0.01006  -0.0055   0.0230   1.0000
  10.750   1.2494   0.01677   0.01048  -0.0036   0.0219   1.0000
  11.000   1.2642   0.01722   0.01094  -0.0017   0.0207   1.0000
  11.250   1.2784   0.01770   0.01143   0.0003   0.0196   1.0000
  11.500   1.2928   0.01814   0.01192   0.0023   0.0187   1.0000
  11.750   1.3062   0.01866   0.01246   0.0043   0.0177   1.0000
  12.000   1.3153   0.01923   0.01306   0.0070   0.0168   1.0000
  12.250   1.3241   0.01994   0.01379   0.0095   0.0160   1.0000
  12.500   1.3357   0.02066   0.01456   0.0112   0.0155   1.0000
  12.750   1.3474   0.02150   0.01545   0.0126   0.0149   1.0000
  13.000   1.3588   0.02246   0.01646   0.0138   0.0142   1.0000
  13.250   1.3695   0.02356   0.01760   0.0149   0.0136   1.0000
  13.500   1.3793   0.02481   0.01889   0.0158   0.0130   1.0000
  13.750   1.3892   0.02613   0.02027   0.0165   0.0125   1.0000
  14.000   1.3995   0.02749   0.02169   0.0171   0.0121   1.0000
  14.250   1.4086   0.02900   0.02326   0.0175   0.0118   1.0000
  14.500   1.4167   0.03067   0.02500   0.0179   0.0114   1.0000
  14.750   1.4236   0.03248   0.02688   0.0182   0.0110   1.0000
  15.000   1.4292   0.03448   0.02893   0.0184   0.0107   1.0000
  15.250   1.4335   0.03666   0.03117   0.0185   0.0104   1.0000
  15.500   1.4359   0.03905   0.03364   0.0185   0.0101   1.0000
  15.750   1.4383   0.04150   0.03616   0.0185   0.0099   1.0000
  16.000   1.4408   0.04397   0.03871   0.0183   0.0097   1.0000
  16.250   1.4418   0.04662   0.04145   0.0181   0.0096   1.0000
  16.500   1.4418   0.04943   0.04435   0.0178   0.0094   1.0000
  16.750   1.4410   0.05243   0.04744   0.0174   0.0092   1.0000
  17.000   1.4393   0.05562   0.05071   0.0168   0.0091   1.0000
  17.250   1.4365   0.05900   0.05418   0.0161   0.0089   1.0000
  17.500   1.4330   0.06259   0.05786   0.0152   0.0088   1.0000
  17.750   1.4284   0.06638   0.06173   0.0142   0.0086   1.0000
  18.000   1.4227   0.07037   0.06580   0.0131   0.0085   1.0000
  18.250   1.4162   0.07457   0.07009   0.0118   0.0083   1.0000
  18.500   1.4086   0.07899   0.07460   0.0104   0.0082   1.0000
  18.750   1.3997   0.08363   0.07934   0.0088   0.0081   1.0000
  19.000   1.3897   0.08854   0.08433   0.0071   0.0080   1.0000
  19.250   1.3784   0.09373   0.08962   0.0051   0.0078   1.0000
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