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NACA 0010-64 (naca001064-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010-64 (naca001064-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.59 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001064-il-1000000-n5.txt
Download as CSV file: xf-naca001064-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-64                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8854   0.16122   0.15940   0.0235   1.0000   0.0064
 -17.500  -1.0072   0.12778   0.12571   0.0059   1.0000   0.0059
 -17.250  -1.2933   0.06451   0.06168  -0.0304   1.0000   0.0049
 -17.000  -1.3230   0.05569   0.05265  -0.0359   1.0000   0.0049
 -16.750  -1.3412   0.04980   0.04658  -0.0388   1.0000   0.0049
 -16.500  -1.3533   0.04534   0.04196  -0.0402   1.0000   0.0049
 -16.250  -1.3617   0.04175   0.03823  -0.0406   1.0000   0.0050
 -16.000  -1.3666   0.03882   0.03515  -0.0403   1.0000   0.0050
 -15.750  -1.3692   0.03634   0.03254  -0.0396   1.0000   0.0051
 -15.500  -1.3694   0.03424   0.03031  -0.0384   1.0000   0.0052
 -15.250  -1.3679   0.03240   0.02834  -0.0369   1.0000   0.0053
 -15.000  -1.3645   0.03079   0.02661  -0.0352   1.0000   0.0053
 -14.750  -1.3594   0.02938   0.02508  -0.0334   1.0000   0.0054
 -14.500  -1.3528   0.02814   0.02372  -0.0314   1.0000   0.0055
 -14.250  -1.3449   0.02700   0.02248  -0.0294   1.0000   0.0056
 -14.000  -1.3387   0.02575   0.02112  -0.0270   1.0000   0.0058
 -13.750  -1.3302   0.02469   0.01995  -0.0247   1.0000   0.0060
 -13.500  -1.3196   0.02376   0.01894  -0.0225   1.0000   0.0063
 -13.250  -1.3059   0.02291   0.01801  -0.0208   1.0000   0.0065
 -13.000  -1.2905   0.02211   0.01712  -0.0193   1.0000   0.0068
 -12.750  -1.2740   0.02136   0.01629  -0.0179   1.0000   0.0070
 -12.500  -1.2568   0.02065   0.01549  -0.0165   1.0000   0.0073
 -12.250  -1.2389   0.01999   0.01475  -0.0152   1.0000   0.0075
 -12.000  -1.2203   0.01937   0.01404  -0.0140   1.0000   0.0077
 -11.750  -1.2025   0.01867   0.01327  -0.0126   1.0000   0.0081
 -11.500  -1.1842   0.01803   0.01258  -0.0113   1.0000   0.0086
 -11.250  -1.1656   0.01747   0.01197  -0.0099   1.0000   0.0091
 -11.000  -1.1469   0.01695   0.01140  -0.0085   1.0000   0.0096
 -10.750  -1.1284   0.01648   0.01087  -0.0070   1.0000   0.0101
 -10.500  -1.1098   0.01603   0.01037  -0.0055   1.0000   0.0107
 -10.250  -1.0915   0.01557   0.00988  -0.0039   1.0000   0.0117
 -10.000  -1.0730   0.01517   0.00947  -0.0023   1.0000   0.0127
  -9.750  -1.0545   0.01481   0.00908  -0.0007   1.0000   0.0136
  -9.500  -1.0334   0.01444   0.00867   0.0004   0.9997   0.0146
  -9.250  -1.0046   0.01409   0.00833  -0.0002   0.9986   0.0161
  -9.000  -0.9754   0.01377   0.00801  -0.0009   0.9973   0.0174
  -8.750  -0.9457   0.01349   0.00768  -0.0016   0.9961   0.0185
  -8.500  -0.9159   0.01317   0.00733  -0.0024   0.9950   0.0194
  -8.250  -0.8863   0.01283   0.00700  -0.0031   0.9938   0.0207
  -8.000  -0.8577   0.01255   0.00672  -0.0036   0.9919   0.0217
  -7.750  -0.8282   0.01229   0.00644  -0.0042   0.9902   0.0228
  -7.500  -0.7980   0.01205   0.00617  -0.0050   0.9886   0.0238
  -7.250  -0.7674   0.01180   0.00589  -0.0058   0.9872   0.0245
  -7.000  -0.7363   0.01158   0.00565  -0.0068   0.9860   0.0250
  -6.750  -0.7055   0.01132   0.00537  -0.0077   0.9847   0.0255
  -6.500  -0.6796   0.01090   0.00491  -0.0075   0.9810   0.0269
  -6.250  -0.6511   0.01059   0.00459  -0.0078   0.9781   0.0281
  -6.000  -0.6218   0.01032   0.00432  -0.0083   0.9756   0.0292
  -5.750  -0.5924   0.01007   0.00405  -0.0088   0.9732   0.0300
  -5.500  -0.5661   0.00985   0.00381  -0.0086   0.9685   0.0307
  -5.250  -0.5380   0.00964   0.00358  -0.0088   0.9647   0.0315
  -5.000  -0.5093   0.00944   0.00336  -0.0090   0.9615   0.0321
  -4.750  -0.4833   0.00926   0.00315  -0.0087   0.9561   0.0326
  -4.500  -0.4561   0.00908   0.00296  -0.0086   0.9511   0.0330
  -4.250  -0.4288   0.00889   0.00275  -0.0085   0.9466   0.0343
  -4.000  -0.4026   0.00870   0.00257  -0.0082   0.9405   0.0368
  -3.750  -0.3759   0.00853   0.00241  -0.0080   0.9348   0.0398
  -3.500  -0.3492   0.00835   0.00226  -0.0078   0.9289   0.0457
  -3.250  -0.3232   0.00813   0.00210  -0.0074   0.9220   0.0612
  -3.000  -0.2968   0.00793   0.00196  -0.0072   0.9157   0.0781
  -2.750  -0.2705   0.00774   0.00183  -0.0069   0.9082   0.0955
  -2.500  -0.2442   0.00754   0.00170  -0.0066   0.9011   0.1195
  -2.250  -0.2181   0.00732   0.00159  -0.0063   0.8929   0.1507
  -2.000  -0.1924   0.00706   0.00147  -0.0060   0.8850   0.1936
  -1.750  -0.1668   0.00679   0.00136  -0.0056   0.8761   0.2410
  -1.500  -0.1414   0.00650   0.00125  -0.0052   0.8672   0.2970
  -1.250  -0.1174   0.00609   0.00113  -0.0046   0.8577   0.3870
  -1.000  -0.0928   0.00575   0.00104  -0.0040   0.8470   0.4621
  -0.750  -0.0680   0.00550   0.00096  -0.0034   0.8327   0.5248
  -0.500  -0.0453   0.00518   0.00089  -0.0024   0.8122   0.6136
  -0.250  -0.0228   0.00496   0.00084  -0.0012   0.7828   0.6880
   0.000   0.0000   0.00493   0.00083   0.0000   0.7386   0.7388
   0.250   0.0230   0.00495   0.00084   0.0012   0.6912   0.7829
   0.500   0.0453   0.00517   0.00089   0.0024   0.6143   0.8121
   0.750   0.0681   0.00549   0.00096   0.0034   0.5272   0.8327
   1.000   0.0928   0.00575   0.00104   0.0040   0.4633   0.8470
   1.250   0.1174   0.00609   0.00113   0.0046   0.3868   0.8577
   1.500   0.1414   0.00650   0.00125   0.0052   0.2989   0.8672
   1.750   0.1668   0.00678   0.00136   0.0056   0.2427   0.8761
   2.000   0.1923   0.00706   0.00147   0.0060   0.1926   0.8850
   2.250   0.2181   0.00732   0.00159   0.0063   0.1503   0.8929
   2.500   0.2442   0.00754   0.00170   0.0066   0.1194   0.9011
   2.750   0.2704   0.00774   0.00183   0.0069   0.0952   0.9082
   3.000   0.2968   0.00793   0.00196   0.0072   0.0782   0.9157
   3.250   0.3232   0.00813   0.00210   0.0074   0.0612   0.9220
   3.500   0.3492   0.00835   0.00225   0.0078   0.0456   0.9289
   3.750   0.3758   0.00853   0.00241   0.0080   0.0398   0.9348
   4.000   0.4026   0.00870   0.00257   0.0082   0.0368   0.9405
   4.250   0.4288   0.00889   0.00275   0.0085   0.0342   0.9465
   4.500   0.4561   0.00908   0.00296   0.0086   0.0330   0.9511
   4.750   0.4833   0.00926   0.00315   0.0087   0.0326   0.9560
   5.000   0.5093   0.00944   0.00336   0.0090   0.0321   0.9615
   5.250   0.5380   0.00964   0.00359   0.0088   0.0315   0.9647
   5.500   0.5661   0.00985   0.00381   0.0086   0.0307   0.9686
   5.750   0.5923   0.01007   0.00405   0.0089   0.0300   0.9733
   6.000   0.6218   0.01032   0.00432   0.0083   0.0292   0.9757
   6.250   0.6512   0.01059   0.00459   0.0078   0.0281   0.9781
   6.500   0.6796   0.01090   0.00491   0.0075   0.0269   0.9810
   6.750   0.7056   0.01132   0.00537   0.0077   0.0255   0.9847
   7.000   0.7364   0.01158   0.00565   0.0068   0.0250   0.9860
   7.250   0.7675   0.01180   0.00590   0.0058   0.0245   0.9873
   7.500   0.7982   0.01205   0.00617   0.0049   0.0238   0.9886
   7.750   0.8284   0.01229   0.00644   0.0042   0.0228   0.9902
   8.000   0.8578   0.01255   0.00672   0.0035   0.0217   0.9920
   8.250   0.8864   0.01283   0.00700   0.0031   0.0207   0.9938
   8.500   0.9160   0.01317   0.00733   0.0024   0.0194   0.9950
   8.750   0.9459   0.01349   0.00768   0.0016   0.0185   0.9961
   9.000   0.9756   0.01378   0.00801   0.0008   0.0174   0.9973
   9.250   1.0048   0.01409   0.00833   0.0002   0.0161   0.9986
   9.500   1.0337   0.01444   0.00867  -0.0005   0.0146   0.9997
   9.750   1.0545   0.01481   0.00908   0.0007   0.0136   1.0000
  10.000   1.0730   0.01517   0.00947   0.0023   0.0127   1.0000
  10.250   1.0915   0.01557   0.00988   0.0039   0.0117   1.0000
  10.500   1.1098   0.01603   0.01037   0.0055   0.0107   1.0000
  10.750   1.1284   0.01648   0.01087   0.0070   0.0101   1.0000
  11.000   1.1470   0.01695   0.01140   0.0085   0.0096   1.0000
  11.250   1.1657   0.01746   0.01196   0.0099   0.0091   1.0000
  11.500   1.1843   0.01803   0.01258   0.0113   0.0086   1.0000
  11.750   1.2026   0.01867   0.01327   0.0126   0.0081   1.0000
  12.000   1.2204   0.01937   0.01404   0.0140   0.0077   1.0000
  12.250   1.2390   0.01998   0.01475   0.0152   0.0075   1.0000
  12.500   1.2569   0.02065   0.01549   0.0165   0.0073   1.0000
  12.750   1.2742   0.02135   0.01629   0.0178   0.0070   1.0000
  13.000   1.2907   0.02211   0.01712   0.0192   0.0068   1.0000
  13.250   1.3062   0.02291   0.01800   0.0207   0.0065   1.0000
  13.500   1.3199   0.02376   0.01894   0.0224   0.0063   1.0000
  13.750   1.3306   0.02469   0.01995   0.0246   0.0060   1.0000
  14.000   1.3391   0.02576   0.02113   0.0269   0.0058   1.0000
  14.250   1.3453   0.02702   0.02250   0.0293   0.0056   1.0000
  14.500   1.3534   0.02814   0.02372   0.0313   0.0055   1.0000
  14.750   1.3601   0.02938   0.02508   0.0332   0.0054   1.0000
  15.000   1.3653   0.03078   0.02660   0.0351   0.0053   1.0000
  15.250   1.3687   0.03239   0.02833   0.0368   0.0053   1.0000
  15.500   1.3705   0.03421   0.03028   0.0382   0.0052   1.0000
  15.750   1.3703   0.03633   0.03253   0.0394   0.0051   1.0000
  16.000   1.3679   0.03880   0.03513   0.0402   0.0050   1.0000
  16.250   1.3631   0.04172   0.03819   0.0404   0.0050   1.0000
  16.500   1.3549   0.04529   0.04191   0.0400   0.0049   1.0000
  16.750   1.3429   0.04974   0.04652   0.0386   0.0049   1.0000
  17.000   1.3252   0.05558   0.05253   0.0357   0.0048   1.0000
  17.250   1.2958   0.06433   0.06150   0.0302   0.0049   1.0000
  17.500   1.0065   0.12838   0.12632  -0.0066   0.0059   1.0000
  17.750   0.8644   0.16764   0.16586  -0.0269   0.0064   1.0000
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