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NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0012-64 (naca001264-il)
Reynolds number: 1,000,000
Max Cl/Cd: 67.75 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001264-il-1000000-n5.txt
Download as CSV file: xf-naca001264-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0012-64                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2592   0.09990   0.09704  -0.0213   1.0000   0.0094
 -19.500  -1.3207   0.08465   0.08153  -0.0298   1.0000   0.0091
 -19.250  -1.3584   0.07423   0.07089  -0.0357   1.0000   0.0091
 -19.000  -1.3837   0.06642   0.06291  -0.0399   1.0000   0.0091
 -18.750  -1.4021   0.06021   0.05655  -0.0429   1.0000   0.0092
 -18.500  -1.4152   0.05511   0.05131  -0.0450   1.0000   0.0093
 -18.250  -1.4247   0.05081   0.04689  -0.0464   1.0000   0.0094
 -18.000  -1.4313   0.04716   0.04312  -0.0473   1.0000   0.0096
 -17.750  -1.4353   0.04401   0.03986  -0.0477   1.0000   0.0098
 -17.500  -1.4372   0.04126   0.03700  -0.0477   1.0000   0.0100
 -17.250  -1.4371   0.03884   0.03447  -0.0474   1.0000   0.0102
 -17.000  -1.4353   0.03669   0.03222  -0.0468   1.0000   0.0105
 -16.750  -1.4318   0.03479   0.03022  -0.0461   1.0000   0.0107
 -16.500  -1.4275   0.03305   0.02838  -0.0452   1.0000   0.0109
 -16.250  -1.4226   0.03140   0.02666  -0.0441   1.0000   0.0114
 -16.000  -1.4158   0.02998   0.02517  -0.0429   1.0000   0.0118
 -15.750  -1.4076   0.02871   0.02384  -0.0416   1.0000   0.0122
 -15.500  -1.3983   0.02756   0.02262  -0.0403   1.0000   0.0127
 -15.250  -1.3881   0.02651   0.02150  -0.0389   1.0000   0.0131
 -15.000  -1.3771   0.02554   0.02045  -0.0375   1.0000   0.0135
 -14.750  -1.3654   0.02466   0.01949  -0.0360   1.0000   0.0138
 -14.500  -1.3531   0.02381   0.01859  -0.0345   1.0000   0.0144
 -14.250  -1.3394   0.02308   0.01783  -0.0331   1.0000   0.0149
 -14.000  -1.3250   0.02242   0.01713  -0.0316   1.0000   0.0155
 -13.750  -1.3100   0.02180   0.01647  -0.0302   1.0000   0.0161
 -13.500  -1.2949   0.02123   0.01583  -0.0287   1.0000   0.0166
 -13.250  -1.2796   0.02068   0.01523  -0.0271   1.0000   0.0171
 -13.000  -1.2646   0.02015   0.01464  -0.0253   1.0000   0.0175
 -12.750  -1.2500   0.01963   0.01409  -0.0235   1.0000   0.0181
 -12.500  -1.2352   0.01920   0.01364  -0.0215   1.0000   0.0186
 -12.250  -1.2217   0.01882   0.01323  -0.0192   1.0000   0.0191
 -12.000  -1.2091   0.01847   0.01284  -0.0166   1.0000   0.0195
 -11.750  -1.1951   0.01812   0.01246  -0.0142   1.0000   0.0200
 -11.500  -1.1811   0.01780   0.01210  -0.0119   1.0000   0.0205
 -11.250  -1.1675   0.01751   0.01176  -0.0093   1.0000   0.0209
 -11.000  -1.1479   0.01719   0.01140  -0.0081   0.9995   0.0213
 -10.750  -1.1208   0.01676   0.01091  -0.0085   0.9981   0.0216
 -10.500  -1.0948   0.01618   0.01031  -0.0087   0.9966   0.0224
 -10.250  -1.0670   0.01576   0.00987  -0.0093   0.9953   0.0230
 -10.000  -1.0382   0.01537   0.00947  -0.0100   0.9942   0.0237
  -9.750  -1.0106   0.01501   0.00908  -0.0104   0.9926   0.0242
  -9.500  -0.9832   0.01466   0.00870  -0.0107   0.9906   0.0248
  -9.250  -0.9549   0.01432   0.00833  -0.0112   0.9888   0.0254
  -9.000  -0.9258   0.01399   0.00797  -0.0118   0.9872   0.0259
  -8.750  -0.8963   0.01368   0.00762  -0.0125   0.9857   0.0263
  -8.500  -0.8670   0.01333   0.00724  -0.0132   0.9843   0.0266
  -8.250  -0.8415   0.01287   0.00676  -0.0131   0.9813   0.0275
  -8.000  -0.8152   0.01251   0.00639  -0.0130   0.9779   0.0282
  -7.750  -0.7877   0.01219   0.00604  -0.0133   0.9751   0.0288
  -7.500  -0.7592   0.01188   0.00572  -0.0137   0.9728   0.0294
  -7.250  -0.7336   0.01161   0.00544  -0.0134   0.9687   0.0300
  -7.000  -0.7078   0.01136   0.00517  -0.0131   0.9644   0.0307
  -6.750  -0.6807   0.01111   0.00490  -0.0131   0.9609   0.0314
  -6.500  -0.6546   0.01088   0.00465  -0.0129   0.9569   0.0319
  -6.250  -0.6292   0.01067   0.00442  -0.0125   0.9518   0.0323
  -6.000  -0.6035   0.01041   0.00415  -0.0121   0.9471   0.0336
  -5.750  -0.5777   0.01018   0.00391  -0.0118   0.9427   0.0351
  -5.500  -0.5523   0.00997   0.00371  -0.0114   0.9371   0.0366
  -5.250  -0.5262   0.00978   0.00351  -0.0110   0.9320   0.0383
  -5.000  -0.5002   0.00958   0.00331  -0.0107   0.9270   0.0415
  -4.750  -0.4746   0.00937   0.00313  -0.0103   0.9209   0.0469
  -4.500  -0.4489   0.00915   0.00294  -0.0099   0.9151   0.0562
  -4.250  -0.4230   0.00895   0.00279  -0.0096   0.9094   0.0664
  -4.000  -0.3970   0.00876   0.00263  -0.0093   0.9028   0.0756
  -3.750  -0.3706   0.00860   0.00248  -0.0090   0.8969   0.0841
  -3.500  -0.3442   0.00843   0.00235  -0.0088   0.8901   0.0944
  -3.250  -0.3182   0.00824   0.00221  -0.0084   0.8833   0.1101
  -3.000  -0.2924   0.00803   0.00208  -0.0081   0.8764   0.1324
  -2.750  -0.2665   0.00782   0.00195  -0.0078   0.8689   0.1572
  -2.500  -0.2410   0.00758   0.00183  -0.0074   0.8618   0.1913
  -2.250  -0.2160   0.00730   0.00171  -0.0069   0.8538   0.2342
  -2.000  -0.1916   0.00698   0.00157  -0.0063   0.8462   0.2911
  -1.750  -0.1682   0.00658   0.00144  -0.0056   0.8377   0.3647
  -1.500  -0.1445   0.00623   0.00132  -0.0049   0.8296   0.4357
  -1.250  -0.1207   0.00591   0.00123  -0.0041   0.8208   0.5026
  -1.000  -0.0968   0.00563   0.00115  -0.0033   0.8110   0.5658
  -0.750  -0.0729   0.00542   0.00110  -0.0025   0.7973   0.6191
  -0.500  -0.0485   0.00529   0.00106  -0.0017   0.7789   0.6616
   0.000   0.0000   0.00521   0.00102   0.0000   0.7268   0.7267
   0.500   0.0485   0.00529   0.00106   0.0017   0.6611   0.7788
   0.750   0.0730   0.00542   0.00110   0.0025   0.6196   0.7974
   1.000   0.0969   0.00562   0.00115   0.0033   0.5666   0.8110
   1.250   0.1205   0.00593   0.00123   0.0041   0.4994   0.8208
   1.500   0.1446   0.00623   0.00132   0.0048   0.4367   0.8296
   1.750   0.1683   0.00658   0.00144   0.0055   0.3653   0.8377
   2.000   0.1916   0.00698   0.00158   0.0063   0.2899   0.8462
   2.250   0.2162   0.00730   0.00170   0.0069   0.2350   0.8538
   2.500   0.2411   0.00758   0.00183   0.0073   0.1909   0.8617
   2.750   0.2666   0.00782   0.00195   0.0077   0.1568   0.8689
   3.000   0.2925   0.00803   0.00208   0.0081   0.1325   0.8763
   3.250   0.3184   0.00824   0.00221   0.0084   0.1101   0.8833
   3.500   0.3444   0.00843   0.00235   0.0087   0.0944   0.8901
   3.750   0.3707   0.00860   0.00248   0.0090   0.0842   0.8969
   4.000   0.3971   0.00876   0.00263   0.0093   0.0756   0.9028
   4.250   0.4231   0.00895   0.00279   0.0096   0.0665   0.9094
   4.500   0.4490   0.00915   0.00294   0.0099   0.0562   0.9151
   4.750   0.4747   0.00938   0.00313   0.0103   0.0469   0.9209
   5.000   0.5003   0.00959   0.00331   0.0107   0.0415   0.9269
   5.250   0.5264   0.00978   0.00351   0.0110   0.0383   0.9319
   5.500   0.5524   0.00997   0.00371   0.0113   0.0366   0.9371
   5.750   0.5778   0.01018   0.00392   0.0117   0.0351   0.9427
   6.000   0.6036   0.01041   0.00415   0.0121   0.0336   0.9471
   6.250   0.6294   0.01067   0.00442   0.0124   0.0323   0.9517
   6.500   0.6547   0.01088   0.00465   0.0128   0.0319   0.9569
   6.750   0.6809   0.01111   0.00490   0.0131   0.0314   0.9609
   7.000   0.7080   0.01136   0.00518   0.0131   0.0307   0.9644
   7.250   0.7338   0.01161   0.00544   0.0133   0.0300   0.9687
   7.500   0.7593   0.01188   0.00572   0.0136   0.0294   0.9727
   7.750   0.7878   0.01219   0.00604   0.0132   0.0288   0.9751
   8.000   0.8153   0.01251   0.00639   0.0130   0.0282   0.9779
   8.250   0.8415   0.01287   0.00676   0.0131   0.0275   0.9813
   8.500   0.8670   0.01333   0.00724   0.0132   0.0266   0.9843
   8.750   0.8963   0.01368   0.00762   0.0125   0.0263   0.9857
   9.000   0.9259   0.01399   0.00797   0.0118   0.0259   0.9873
   9.250   0.9550   0.01431   0.00833   0.0112   0.0254   0.9888
   9.500   0.9833   0.01466   0.00870   0.0106   0.0248   0.9907
   9.750   1.0108   0.01501   0.00907   0.0103   0.0242   0.9927
  10.000   1.0383   0.01537   0.00947   0.0099   0.0237   0.9942
  10.250   1.0671   0.01575   0.00987   0.0093   0.0230   0.9953
  10.500   1.0949   0.01618   0.01031   0.0087   0.0223   0.9966
  10.750   1.1210   0.01675   0.01091   0.0085   0.0216   0.9981
  11.000   1.1481   0.01718   0.01139   0.0081   0.0213   0.9995
  11.250   1.1674   0.01751   0.01176   0.0094   0.0209   1.0000
  11.500   1.1811   0.01780   0.01210   0.0119   0.0205   1.0000
  11.750   1.1951   0.01812   0.01246   0.0142   0.0200   1.0000
  12.000   1.2093   0.01846   0.01284   0.0165   0.0195   1.0000
  12.250   1.2220   0.01882   0.01323   0.0191   0.0191   1.0000
  12.500   1.2357   0.01920   0.01364   0.0214   0.0186   1.0000
  12.750   1.2505   0.01963   0.01409   0.0234   0.0181   1.0000
  13.000   1.2652   0.02015   0.01464   0.0252   0.0175   1.0000
  13.250   1.2803   0.02068   0.01522   0.0269   0.0171   1.0000
  13.500   1.2958   0.02122   0.01582   0.0285   0.0166   1.0000
  13.750   1.3110   0.02179   0.01646   0.0300   0.0160   1.0000
  14.000   1.3260   0.02241   0.01712   0.0315   0.0155   1.0000
  14.250   1.3404   0.02307   0.01782   0.0329   0.0149   1.0000
  14.500   1.3542   0.02380   0.01859   0.0343   0.0143   1.0000
  14.750   1.3665   0.02465   0.01948   0.0358   0.0138   1.0000
  15.000   1.3784   0.02554   0.02044   0.0373   0.0135   1.0000
  15.250   1.3894   0.02650   0.02149   0.0387   0.0131   1.0000
  15.500   1.3997   0.02755   0.02261   0.0401   0.0127   1.0000
  15.750   1.4091   0.02870   0.02382   0.0414   0.0122   1.0000
  16.000   1.4174   0.02996   0.02515   0.0426   0.0118   1.0000
  16.250   1.4243   0.03138   0.02664   0.0438   0.0114   1.0000
  16.500   1.4294   0.03302   0.02836   0.0448   0.0110   1.0000
  16.750   1.4338   0.03477   0.03020   0.0458   0.0107   1.0000
  17.000   1.4374   0.03666   0.03219   0.0465   0.0105   1.0000
  17.250   1.4393   0.03880   0.03443   0.0470   0.0102   1.0000
  17.500   1.4395   0.04121   0.03695   0.0473   0.0100   1.0000
  17.750   1.4377   0.04396   0.03981   0.0473   0.0098   1.0000
  18.000   1.4339   0.04710   0.04306   0.0469   0.0096   1.0000
  18.250   1.4273   0.05075   0.04682   0.0461   0.0094   1.0000
  18.500   1.4180   0.05502   0.05123   0.0446   0.0093   1.0000
  18.750   1.4049   0.06013   0.05647   0.0425   0.0092   1.0000
  19.000   1.3867   0.06634   0.06283   0.0395   0.0091   1.0000
  19.250   1.3615   0.07414   0.07081   0.0352   0.0091   1.0000
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