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NACA 0010 (naca0010-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010 (naca0010-il)
Reynolds number: 500,000
Max Cl/Cd: 57.81 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca0010-il-500000-n5.txt
Download as CSV file: xf-naca0010-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.0427   0.12024   0.11753   0.0178   1.0000   0.0088
 -16.500  -1.0976   0.10476   0.10188   0.0097   1.0000   0.0086
 -16.250  -1.1470   0.09107   0.08801   0.0023   1.0000   0.0084
 -16.000  -1.1881   0.07916   0.07590  -0.0044   1.0000   0.0082
 -15.750  -1.2206   0.06892   0.06547  -0.0106   1.0000   0.0081
 -15.500  -1.2444   0.06048   0.05683  -0.0161   1.0000   0.0081
 -15.250  -1.2616   0.05357   0.04973  -0.0206   1.0000   0.0082
 -15.000  -1.2731   0.04808   0.04407  -0.0240   1.0000   0.0082
 -14.750  -1.2810   0.04366   0.03948  -0.0262   1.0000   0.0083
 -14.500  -1.2855   0.04014   0.03581  -0.0274   1.0000   0.0085
 -14.250  -1.2878   0.03728   0.03279  -0.0277   1.0000   0.0086
 -14.000  -1.2880   0.03492   0.03028  -0.0272   1.0000   0.0088
 -13.750  -1.2866   0.03293   0.02815  -0.0261   1.0000   0.0090
 -13.500  -1.2833   0.03126   0.02633  -0.0245   1.0000   0.0092
 -13.250  -1.2784   0.02981   0.02473  -0.0226   1.0000   0.0094
 -13.000  -1.2715   0.02855   0.02333  -0.0205   1.0000   0.0097
 -12.750  -1.2605   0.02741   0.02205  -0.0188   1.0000   0.0099
 -12.500  -1.2493   0.02612   0.02065  -0.0172   1.0000   0.0104
 -12.250  -1.2343   0.02509   0.01954  -0.0160   1.0000   0.0109
 -12.000  -1.2173   0.02420   0.01858  -0.0149   1.0000   0.0115
 -11.750  -1.1994   0.02336   0.01764  -0.0139   1.0000   0.0121
 -11.500  -1.1808   0.02254   0.01670  -0.0129   1.0000   0.0127
 -11.250  -1.1616   0.02174   0.01577  -0.0119   1.0000   0.0132
 -11.000  -1.1423   0.02091   0.01488  -0.0110   1.0000   0.0140
 -10.750  -1.1210   0.02028   0.01421  -0.0103   1.0000   0.0149
 -10.500  -1.0990   0.01973   0.01361  -0.0096   1.0000   0.0159
 -10.250  -1.0767   0.01919   0.01299  -0.0089   1.0000   0.0170
 -10.000  -1.0545   0.01862   0.01234  -0.0082   1.0000   0.0180
  -9.750  -1.0318   0.01811   0.01180  -0.0076   1.0000   0.0192
  -9.500  -1.0083   0.01769   0.01134  -0.0071   1.0000   0.0205
  -9.250  -0.9848   0.01725   0.01084  -0.0065   1.0000   0.0218
  -9.000  -0.9608   0.01688   0.01039  -0.0060   1.0000   0.0229
  -8.750  -0.9380   0.01635   0.00981  -0.0053   1.0000   0.0240
  -8.500  -0.9150   0.01584   0.00926  -0.0046   1.0000   0.0254
  -8.250  -0.8913   0.01543   0.00883  -0.0040   1.0000   0.0267
  -8.000  -0.8675   0.01506   0.00841  -0.0034   1.0000   0.0280
  -7.750  -0.8435   0.01471   0.00800  -0.0027   1.0000   0.0292
  -7.500  -0.8195   0.01439   0.00763  -0.0021   1.0000   0.0300
  -7.250  -0.7972   0.01385   0.00705  -0.0012   1.0000   0.0315
  -7.000  -0.7744   0.01341   0.00659  -0.0003   1.0000   0.0330
  -6.750  -0.7513   0.01305   0.00621   0.0005   1.0000   0.0345
  -6.500  -0.7280   0.01273   0.00586   0.0014   1.0000   0.0359
  -6.250  -0.7046   0.01242   0.00551   0.0022   1.0000   0.0371
  -6.000  -0.6812   0.01214   0.00519   0.0030   1.0000   0.0382
  -5.750  -0.6582   0.01180   0.00483   0.0040   1.0000   0.0400
  -5.500  -0.6352   0.01148   0.00451   0.0049   1.0000   0.0424
  -5.250  -0.6121   0.01121   0.00424   0.0058   1.0000   0.0452
  -5.000  -0.5834   0.01095   0.00397   0.0055   0.9986   0.0491
  -4.750  -0.5495   0.01062   0.00369   0.0040   0.9957   0.0594
  -4.500  -0.5162   0.01026   0.00343   0.0026   0.9925   0.0765
  -4.250  -0.4831   0.00994   0.00318   0.0013   0.9886   0.0953
  -4.000  -0.4488   0.00962   0.00296  -0.0002   0.9853   0.1173
  -3.750  -0.4169   0.00931   0.00276  -0.0012   0.9800   0.1429
  -3.500  -0.3841   0.00899   0.00256  -0.0024   0.9747   0.1722
  -3.250  -0.3533   0.00869   0.00239  -0.0032   0.9673   0.2033
  -3.000  -0.3212   0.00837   0.00222  -0.0042   0.9602   0.2419
  -2.750  -0.2920   0.00803   0.00208  -0.0046   0.9499   0.2895
  -2.500  -0.2631   0.00770   0.00194  -0.0048   0.9384   0.3398
  -2.250  -0.2348   0.00742   0.00182  -0.0049   0.9246   0.3849
  -2.000  -0.2075   0.00718   0.00171  -0.0047   0.9082   0.4282
  -1.750  -0.1810   0.00699   0.00162  -0.0043   0.8895   0.4653
  -1.500  -0.1550   0.00681   0.00153  -0.0037   0.8687   0.5057
  -1.250  -0.1293   0.00665   0.00146  -0.0031   0.8455   0.5472
  -0.750  -0.0775   0.00649   0.00135  -0.0018   0.7945   0.6116
  -0.500  -0.0517   0.00644   0.00131  -0.0012   0.7661   0.6436
  -0.250  -0.0258   0.00641   0.00129  -0.0006   0.7368   0.6754
   0.000   0.0000   0.00640   0.00129   0.0000   0.7063   0.7064
   0.250   0.0259   0.00641   0.00129   0.0006   0.6753   0.7366
   0.500   0.0517   0.00644   0.00131   0.0012   0.6434   0.7662
   0.750   0.0775   0.00650   0.00135   0.0018   0.6114   0.7944
   1.250   0.1293   0.00665   0.00146   0.0031   0.5474   0.8455
   1.500   0.1550   0.00681   0.00153   0.0037   0.5059   0.8687
   1.750   0.1810   0.00699   0.00162   0.0043   0.4652   0.8893
   2.000   0.2075   0.00718   0.00171   0.0047   0.4278   0.9082
   2.250   0.2348   0.00742   0.00182   0.0049   0.3851   0.9246
   2.500   0.2631   0.00770   0.00194   0.0048   0.3396   0.9383
   2.750   0.2920   0.00803   0.00208   0.0046   0.2895   0.9499
   3.000   0.3211   0.00837   0.00222   0.0042   0.2419   0.9603
   3.250   0.3533   0.00869   0.00239   0.0032   0.2035   0.9673
   3.500   0.3841   0.00899   0.00256   0.0024   0.1722   0.9747
   3.750   0.4169   0.00930   0.00276   0.0012   0.1429   0.9800
   4.000   0.4488   0.00961   0.00296   0.0002   0.1174   0.9853
   4.250   0.4831   0.00994   0.00318  -0.0014   0.0954   0.9886
   4.500   0.5162   0.01026   0.00343  -0.0026   0.0765   0.9925
   4.750   0.5496   0.01061   0.00369  -0.0040   0.0594   0.9957
   5.000   0.5834   0.01095   0.00397  -0.0055   0.0491   0.9986
   5.250   0.6121   0.01121   0.00424  -0.0058   0.0452   1.0000
   5.500   0.6352   0.01148   0.00451  -0.0049   0.0425   1.0000
   5.750   0.6582   0.01180   0.00483  -0.0040   0.0400   1.0000
   6.000   0.6812   0.01214   0.00519  -0.0030   0.0382   1.0000
   6.250   0.7046   0.01242   0.00551  -0.0022   0.0371   1.0000
   6.500   0.7280   0.01273   0.00586  -0.0013   0.0359   1.0000
   6.750   0.7512   0.01305   0.00621  -0.0005   0.0345   1.0000
   7.000   0.7744   0.01341   0.00659   0.0003   0.0330   1.0000
   7.250   0.7972   0.01385   0.00705   0.0012   0.0315   1.0000
   7.500   0.8195   0.01439   0.00763   0.0021   0.0300   1.0000
   7.750   0.8435   0.01471   0.00800   0.0027   0.0292   1.0000
   8.000   0.8675   0.01506   0.00841   0.0034   0.0280   1.0000
   8.250   0.8913   0.01543   0.00883   0.0040   0.0267   1.0000
   8.500   0.9151   0.01583   0.00926   0.0046   0.0254   1.0000
   8.750   0.9380   0.01635   0.00980   0.0053   0.0240   1.0000
   9.000   0.9609   0.01687   0.01038   0.0060   0.0229   1.0000
   9.250   0.9848   0.01725   0.01084   0.0065   0.0218   1.0000
   9.500   1.0083   0.01769   0.01134   0.0071   0.0205   1.0000
   9.750   1.0318   0.01811   0.01180   0.0076   0.0192   1.0000
  10.000   1.0545   0.01862   0.01234   0.0082   0.0180   1.0000
  10.250   1.0767   0.01919   0.01299   0.0089   0.0170   1.0000
  10.500   1.0990   0.01973   0.01361   0.0096   0.0159   1.0000
  10.750   1.1211   0.02028   0.01421   0.0103   0.0149   1.0000
  11.000   1.1423   0.02091   0.01488   0.0110   0.0140   1.0000
  11.250   1.1616   0.02174   0.01577   0.0119   0.0132   1.0000
  11.500   1.1809   0.02254   0.01670   0.0129   0.0127   1.0000
  11.750   1.1995   0.02336   0.01764   0.0139   0.0120   1.0000
  12.000   1.2175   0.02420   0.01857   0.0149   0.0115   1.0000
  12.250   1.2346   0.02509   0.01954   0.0159   0.0109   1.0000
  12.500   1.2496   0.02612   0.02065   0.0172   0.0104   1.0000
  12.750   1.2609   0.02741   0.02205   0.0187   0.0099   1.0000
  13.000   1.2719   0.02855   0.02333   0.0204   0.0097   1.0000
  13.250   1.2789   0.02981   0.02473   0.0225   0.0094   1.0000
  13.500   1.2839   0.03126   0.02633   0.0244   0.0092   1.0000
  13.750   1.2872   0.03294   0.02815   0.0260   0.0090   1.0000
  14.000   1.2888   0.03491   0.03027   0.0271   0.0088   1.0000
  14.250   1.2886   0.03726   0.03277   0.0275   0.0086   1.0000
  14.500   1.2865   0.04012   0.03579   0.0273   0.0085   1.0000
  14.750   1.2820   0.04365   0.03947   0.0261   0.0083   1.0000
  15.000   1.2744   0.04805   0.04403   0.0238   0.0082   1.0000
  15.250   1.2628   0.05356   0.04972   0.0204   0.0082   1.0000
  15.500   1.2460   0.06043   0.05678   0.0159   0.0081   1.0000
  15.750   1.2223   0.06887   0.06541   0.0104   0.0081   1.0000
  16.000   1.1898   0.07913   0.07587   0.0042   0.0082   1.0000
  16.250   1.1483   0.09115   0.08809  -0.0026   0.0084   1.0000
  16.500   1.0990   0.10483   0.10196  -0.0100   0.0086   1.0000
  16.750   1.0437   0.12041   0.11770  -0.0182   0.0088   1.0000
  17.000   0.9647   0.14290   0.14040  -0.0300   0.0092   1.0000
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