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NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 0012-64 (naca001264-il)
Reynolds number: 500,000
Max Cl/Cd: 53.21 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001264-il-500000-n5.txt
Download as CSV file: xf-naca001264-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1137   0.10212   0.09899  -0.0206   1.0000   0.0147
 -18.000  -1.1675   0.08763   0.08425  -0.0288   1.0000   0.0145
 -17.750  -1.2008   0.07746   0.07387  -0.0347   1.0000   0.0145
 -17.500  -1.2231   0.06970   0.06593  -0.0391   1.0000   0.0145
 -17.250  -1.2384   0.06357   0.05964  -0.0424   1.0000   0.0147
 -17.000  -1.2488   0.05858   0.05452  -0.0448   1.0000   0.0148
 -16.750  -1.2555   0.05443   0.05023  -0.0465   1.0000   0.0151
 -16.500  -1.2595   0.05090   0.04657  -0.0476   1.0000   0.0154
 -16.250  -1.2619   0.04775   0.04329  -0.0482   1.0000   0.0157
 -16.000  -1.2626   0.04497   0.04037  -0.0485   1.0000   0.0160
 -15.750  -1.2620   0.04247   0.03774  -0.0485   1.0000   0.0164
 -15.500  -1.2603   0.04020   0.03533  -0.0481   1.0000   0.0168
 -15.250  -1.2571   0.03816   0.03314  -0.0475   1.0000   0.0172
 -15.000  -1.2537   0.03627   0.03113  -0.0466   1.0000   0.0175
 -14.750  -1.2480   0.03467   0.02947  -0.0457   1.0000   0.0179
 -14.500  -1.2400   0.03334   0.02806  -0.0447   1.0000   0.0182
 -14.250  -1.2306   0.03216   0.02680  -0.0436   1.0000   0.0186
 -14.000  -1.2206   0.03106   0.02561  -0.0424   1.0000   0.0191
 -13.750  -1.2102   0.03002   0.02448  -0.0411   1.0000   0.0196
 -13.500  -1.1992   0.02904   0.02339  -0.0397   1.0000   0.0201
 -13.250  -1.1876   0.02811   0.02236  -0.0382   1.0000   0.0207
 -13.000  -1.1752   0.02726   0.02138  -0.0367   1.0000   0.0212
 -12.750  -1.1627   0.02644   0.02045  -0.0351   1.0000   0.0216
 -12.500  -1.1532   0.02544   0.01940  -0.0330   1.0000   0.0221
 -12.250  -1.1411   0.02470   0.01861  -0.0312   1.0000   0.0225
 -12.000  -1.1278   0.02409   0.01795  -0.0293   1.0000   0.0230
 -11.750  -1.1147   0.02354   0.01734  -0.0273   1.0000   0.0236
 -11.500  -1.1023   0.02301   0.01675  -0.0250   1.0000   0.0242
 -11.250  -1.0912   0.02250   0.01617  -0.0223   1.0000   0.0247
 -11.000  -1.0805   0.02201   0.01560  -0.0195   1.0000   0.0253
 -10.750  -1.0679   0.02152   0.01503  -0.0170   1.0000   0.0257
 -10.500  -1.0548   0.02110   0.01453  -0.0145   1.0000   0.0262
 -10.250  -1.0425   0.02064   0.01400  -0.0119   1.0000   0.0266
 -10.000  -1.0339   0.01992   0.01325  -0.0086   1.0000   0.0272
  -9.750  -1.0231   0.01941   0.01270  -0.0057   1.0000   0.0278
  -9.500  -1.0086   0.01896   0.01223  -0.0034   0.9998   0.0284
  -9.250  -0.9809   0.01844   0.01167  -0.0040   0.9980   0.0291
  -9.000  -0.9528   0.01793   0.01110  -0.0046   0.9962   0.0299
  -8.750  -0.9242   0.01741   0.01054  -0.0053   0.9945   0.0306
  -8.500  -0.8960   0.01695   0.01001  -0.0058   0.9927   0.0314
  -8.250  -0.8684   0.01651   0.00951  -0.0062   0.9902   0.0320
  -8.000  -0.8401   0.01603   0.00898  -0.0067   0.9880   0.0324
  -7.750  -0.8121   0.01540   0.00832  -0.0073   0.9859   0.0334
  -7.500  -0.7822   0.01491   0.00782  -0.0082   0.9844   0.0344
  -7.250  -0.7536   0.01451   0.00740  -0.0087   0.9820   0.0355
  -7.000  -0.7258   0.01413   0.00700  -0.0090   0.9789   0.0365
  -6.750  -0.6960   0.01377   0.00660  -0.0097   0.9766   0.0375
  -6.500  -0.6655   0.01342   0.00622  -0.0106   0.9745   0.0385
  -6.250  -0.6346   0.01307   0.00585  -0.0115   0.9727   0.0398
  -6.000  -0.6084   0.01272   0.00551  -0.0114   0.9687   0.0419
  -5.750  -0.5809   0.01241   0.00520  -0.0115   0.9649   0.0444
  -5.500  -0.5515   0.01212   0.00492  -0.0120   0.9619   0.0478
  -5.250  -0.5219   0.01179   0.00463  -0.0126   0.9594   0.0544
  -5.000  -0.4973   0.01152   0.00439  -0.0121   0.9539   0.0626
  -4.750  -0.4703   0.01124   0.00416  -0.0120   0.9495   0.0723
  -4.500  -0.4419   0.01098   0.00392  -0.0123   0.9460   0.0826
  -4.000  -0.3906   0.01047   0.00353  -0.0116   0.9354   0.1089
  -3.750  -0.3639   0.01016   0.00331  -0.0115   0.9309   0.1310
  -3.500  -0.3389   0.00986   0.00314  -0.0110   0.9254   0.1596
  -3.250  -0.3143   0.00955   0.00296  -0.0105   0.9191   0.1928
  -3.000  -0.2888   0.00920   0.00276  -0.0101   0.9140   0.2335
  -2.750  -0.2667   0.00874   0.00257  -0.0091   0.9070   0.2986
  -2.500  -0.2450   0.00819   0.00236  -0.0081   0.9004   0.3850
  -2.250  -0.2248   0.00762   0.00218  -0.0067   0.8936   0.4837
  -2.000  -0.2037   0.00718   0.00205  -0.0053   0.8862   0.5641
  -1.750  -0.1802   0.00690   0.00197  -0.0044   0.8797   0.6175
  -1.500  -0.1555   0.00673   0.00191  -0.0036   0.8721   0.6542
  -1.250  -0.1301   0.00657   0.00187  -0.0030   0.8656   0.6928
  -1.000  -0.1052   0.00644   0.00187  -0.0022   0.8575   0.7276
  -0.750  -0.0787   0.00636   0.00185  -0.0017   0.8505   0.7541
  -0.500  -0.0528   0.00630   0.00188  -0.0011   0.8419   0.7792
  -0.250  -0.0263   0.00627   0.00188  -0.0006   0.8329   0.8017
   0.000   0.0000   0.00626   0.00188   0.0000   0.8196   0.8196
   0.250   0.0264   0.00627   0.00188   0.0006   0.8018   0.8329
   0.500   0.0529   0.00630   0.00188   0.0011   0.7793   0.8419
   0.750   0.0788   0.00636   0.00185   0.0017   0.7537   0.8505
   1.000   0.1053   0.00644   0.00187   0.0022   0.7275   0.8575
   1.250   0.1302   0.00657   0.00187   0.0029   0.6928   0.8656
   1.500   0.1555   0.00673   0.00191   0.0036   0.6542   0.8721
   1.750   0.1803   0.00690   0.00197   0.0044   0.6180   0.8797
   2.000   0.2037   0.00718   0.00205   0.0053   0.5637   0.8862
   2.250   0.2248   0.00762   0.00218   0.0067   0.4839   0.8936
   2.500   0.2450   0.00819   0.00236   0.0081   0.3851   0.9004
   2.750   0.2668   0.00874   0.00257   0.0091   0.2983   0.9070
   3.000   0.2889   0.00920   0.00276   0.0101   0.2336   0.9140
   3.250   0.3144   0.00955   0.00296   0.0104   0.1928   0.9190
   3.500   0.3390   0.00986   0.00314   0.0110   0.1597   0.9253
   3.750   0.3639   0.01016   0.00331   0.0115   0.1310   0.9309
   4.000   0.3907   0.01047   0.00353   0.0116   0.1090   0.9354
   4.500   0.4419   0.01098   0.00392   0.0123   0.0826   0.9460
   4.750   0.4704   0.01124   0.00416   0.0120   0.0723   0.9495
   5.000   0.4973   0.01152   0.00439   0.0121   0.0626   0.9540
   5.250   0.5219   0.01179   0.00462   0.0126   0.0545   0.9594
   5.500   0.5515   0.01212   0.00491   0.0120   0.0479   0.9619
   5.750   0.5810   0.01241   0.00520   0.0115   0.0444   0.9649
   6.000   0.6085   0.01272   0.00551   0.0114   0.0419   0.9687
   6.250   0.6347   0.01307   0.00585   0.0115   0.0398   0.9727
   6.500   0.6656   0.01342   0.00622   0.0106   0.0385   0.9745
   6.750   0.6960   0.01376   0.00660   0.0097   0.0375   0.9766
   7.000   0.7258   0.01413   0.00700   0.0090   0.0365   0.9790
   7.250   0.7536   0.01451   0.00740   0.0087   0.0355   0.9821
   7.500   0.7822   0.01491   0.00782   0.0082   0.0344   0.9844
   7.750   0.8121   0.01540   0.00832   0.0073   0.0334   0.9859
   8.000   0.8401   0.01603   0.00898   0.0067   0.0324   0.9880
   8.250   0.8684   0.01650   0.00951   0.0062   0.0320   0.9903
   8.500   0.8961   0.01695   0.01001   0.0058   0.0314   0.9927
   8.750   0.9243   0.01741   0.01054   0.0053   0.0306   0.9946
   9.000   0.9530   0.01793   0.01110   0.0046   0.0299   0.9962
   9.250   0.9811   0.01845   0.01167   0.0039   0.0291   0.9981
   9.500   1.0088   0.01896   0.01223   0.0034   0.0284   0.9998
   9.750   1.0230   0.01941   0.01270   0.0057   0.0278   1.0000
  10.000   1.0339   0.01992   0.01325   0.0086   0.0272   1.0000
  10.250   1.0425   0.02064   0.01400   0.0119   0.0266   1.0000
  10.500   1.0548   0.02109   0.01453   0.0145   0.0262   1.0000
  10.750   1.0680   0.02152   0.01503   0.0170   0.0257   1.0000
  11.000   1.0806   0.02201   0.01559   0.0195   0.0253   1.0000
  11.250   1.0915   0.02250   0.01617   0.0223   0.0247   1.0000
  11.500   1.1027   0.02300   0.01674   0.0249   0.0242   1.0000
  11.750   1.1152   0.02353   0.01733   0.0272   0.0236   1.0000
  12.000   1.1284   0.02409   0.01794   0.0292   0.0230   1.0000
  12.250   1.1417   0.02470   0.01861   0.0310   0.0225   1.0000
  12.500   1.1539   0.02544   0.01939   0.0329   0.0221   1.0000
  12.750   1.1633   0.02644   0.02046   0.0350   0.0216   1.0000
  13.000   1.1760   0.02726   0.02138   0.0366   0.0212   1.0000
  13.250   1.1885   0.02811   0.02236   0.0381   0.0207   1.0000
  13.500   1.2002   0.02904   0.02339   0.0395   0.0201   1.0000
  13.750   1.2113   0.03001   0.02447   0.0409   0.0196   1.0000
  14.000   1.2219   0.03104   0.02559   0.0422   0.0191   1.0000
  14.250   1.2319   0.03214   0.02678   0.0434   0.0186   1.0000
  14.500   1.2414   0.03332   0.02804   0.0445   0.0182   1.0000
  14.750   1.2495   0.03465   0.02944   0.0455   0.0179   1.0000
  15.000   1.2552   0.03625   0.03111   0.0464   0.0175   1.0000
  15.250   1.2588   0.03814   0.03312   0.0472   0.0171   1.0000
  15.500   1.2620   0.04018   0.03531   0.0478   0.0168   1.0000
  15.750   1.2639   0.04243   0.03771   0.0482   0.0164   1.0000
  16.000   1.2646   0.04493   0.04034   0.0482   0.0160   1.0000
  16.250   1.2643   0.04768   0.04322   0.0479   0.0156   1.0000
  16.500   1.2623   0.05077   0.04643   0.0473   0.0153   1.0000
  16.750   1.2583   0.05431   0.05011   0.0462   0.0150   1.0000
  17.000   1.2514   0.05849   0.05443   0.0445   0.0148   1.0000
  17.250   1.2413   0.06344   0.05951   0.0421   0.0146   1.0000
  17.500   1.2261   0.06956   0.06578   0.0388   0.0145   1.0000
  17.750   1.2040   0.07730   0.07370   0.0343   0.0144   1.0000
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