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NACA 2410 (naca2410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 2410 (naca2410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.73 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca2410-il-1000000-n5.txt
Download as CSV file: xf-naca2410-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 2410                                       
  
 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  -0.9011   0.10848   0.10636  -0.0108   1.0000   0.0069
 -15.500  -1.0391   0.07950   0.07709  -0.0278   1.0000   0.0063
 -15.250  -1.2124   0.03950   0.03642  -0.0604   1.0000   0.0057
 -15.000  -1.2259   0.03501   0.03174  -0.0631   1.0000   0.0057
 -14.750  -1.2312   0.03253   0.02911  -0.0623   1.0000   0.0058
 -14.500  -1.2286   0.03066   0.02710  -0.0610   1.0000   0.0058
 -14.250  -1.2195   0.02907   0.02537  -0.0601   1.0000   0.0059
 -14.000  -1.2073   0.02768   0.02386  -0.0593   1.0000   0.0060
 -13.750  -1.1966   0.02601   0.02205  -0.0583   1.0000   0.0062
 -13.500  -1.1824   0.02466   0.02057  -0.0574   1.0000   0.0064
 -13.250  -1.1661   0.02352   0.01933  -0.0565   1.0000   0.0066
 -13.000  -1.1485   0.02251   0.01823  -0.0557   1.0000   0.0068
 -12.750  -1.1301   0.02160   0.01723  -0.0548   1.0000   0.0070
 -12.500  -1.1112   0.02075   0.01629  -0.0539   1.0000   0.0072
 -12.250  -1.0920   0.01998   0.01542  -0.0529   1.0000   0.0075
 -12.000  -1.0728   0.01925   0.01461  -0.0518   1.0000   0.0077
 -11.750  -1.0533   0.01858   0.01384  -0.0507   1.0000   0.0079
 -11.500  -1.0334   0.01796   0.01314  -0.0496   1.0000   0.0081
 -11.250  -1.0142   0.01727   0.01237  -0.0484   1.0000   0.0084
 -11.000  -0.9949   0.01661   0.01165  -0.0471   1.0000   0.0088
 -10.750  -0.9752   0.01604   0.01102  -0.0459   1.0000   0.0092
 -10.500  -0.9495   0.01547   0.01040  -0.0459   0.9993   0.0096
 -10.250  -0.9199   0.01494   0.00979  -0.0467   0.9980   0.0102
 -10.000  -0.8898   0.01446   0.00924  -0.0475   0.9966   0.0107
  -9.750  -0.8596   0.01390   0.00864  -0.0483   0.9953   0.0115
  -9.500  -0.8290   0.01341   0.00811  -0.0493   0.9941   0.0125
  -9.250  -0.7998   0.01299   0.00765  -0.0498   0.9921   0.0134
  -9.000  -0.7696   0.01260   0.00720  -0.0505   0.9901   0.0141
  -8.750  -0.7389   0.01219   0.00679  -0.0514   0.9884   0.0157
  -8.500  -0.7074   0.01185   0.00644  -0.0524   0.9868   0.0172
  -8.250  -0.6758   0.01154   0.00609  -0.0533   0.9852   0.0186
  -8.000  -0.6467   0.01124   0.00580  -0.0537   0.9819   0.0204
  -7.750  -0.6170   0.01099   0.00554  -0.0542   0.9783   0.0219
  -7.500  -0.5860   0.01075   0.00527  -0.0550   0.9751   0.0231
  -7.250  -0.5571   0.01053   0.00501  -0.0552   0.9697   0.0239
  -7.000  -0.5280   0.01021   0.00468  -0.0555   0.9637   0.0256
  -6.750  -0.4999   0.00997   0.00443  -0.0556   0.9573   0.0269
  -6.500  -0.4720   0.00977   0.00420  -0.0556   0.9504   0.0281
  -6.250  -0.4443   0.00958   0.00398  -0.0555   0.9436   0.0291
  -6.000  -0.4169   0.00940   0.00376  -0.0553   0.9355   0.0298
  -5.750  -0.3895   0.00923   0.00354  -0.0552   0.9274   0.0305
  -5.500  -0.3626   0.00896   0.00323  -0.0549   0.9183   0.0322
  -5.250  -0.3355   0.00876   0.00300  -0.0547   0.9087   0.0337
  -5.000  -0.3083   0.00859   0.00279  -0.0545   0.8986   0.0352
  -4.750  -0.2811   0.00844   0.00260  -0.0542   0.8875   0.0364
  -4.500  -0.2536   0.00831   0.00242  -0.0541   0.8758   0.0374
  -4.250  -0.2262   0.00819   0.00224  -0.0539   0.8635   0.0386
  -4.000  -0.1988   0.00804   0.00206  -0.0537   0.8506   0.0422
  -3.750  -0.1714   0.00792   0.00191  -0.0535   0.8370   0.0461
  -3.500  -0.1441   0.00779   0.00177  -0.0533   0.8226   0.0537
  -3.250  -0.1168   0.00766   0.00163  -0.0532   0.8075   0.0658
  -3.000  -0.0894   0.00755   0.00152  -0.0530   0.7919   0.0794
  -2.750  -0.0619   0.00745   0.00142  -0.0529   0.7759   0.0926
  -2.500  -0.0344   0.00737   0.00132  -0.0527   0.7589   0.1069
  -2.250  -0.0069   0.00729   0.00124  -0.0526   0.7420   0.1233
  -2.000   0.0206   0.00723   0.00117  -0.0525   0.7245   0.1415
  -1.750   0.0480   0.00715   0.00111  -0.0524   0.7071   0.1628
  -1.250   0.1028   0.00695   0.00101  -0.0522   0.6720   0.2321
  -1.000   0.1303   0.00688   0.00098  -0.0522   0.6538   0.2630
  -0.750   0.1579   0.00684   0.00096  -0.0521   0.6358   0.2894
  -0.250   0.2125   0.00665   0.00094  -0.0520   0.6002   0.3830
   0.000   0.2398   0.00658   0.00095  -0.0519   0.5828   0.4290
   0.250   0.2668   0.00646   0.00096  -0.0518   0.5656   0.4950
   0.500   0.2936   0.00631   0.00099  -0.0516   0.5484   0.5720
   0.750   0.3207   0.00623   0.00103  -0.0515   0.5316   0.6289
   1.000   0.3477   0.00618   0.00108  -0.0513   0.5157   0.6801
   1.250   0.3745   0.00613   0.00113  -0.0510   0.5001   0.7301
   1.500   0.4007   0.00607   0.00119  -0.0506   0.4841   0.7846
   1.750   0.4262   0.00601   0.00127  -0.0500   0.4685   0.8423
   2.000   0.4506   0.00601   0.00136  -0.0490   0.4507   0.8950
   2.250   0.4751   0.00616   0.00146  -0.0481   0.4154   0.9381
   2.500   0.5050   0.00643   0.00157  -0.0486   0.3720   0.9664
   2.750   0.5375   0.00669   0.00168  -0.0497   0.3371   0.9825
   3.000   0.5706   0.00692   0.00179  -0.0509   0.3096   0.9926
   3.250   0.6045   0.00722   0.00194  -0.0525   0.2735   1.0000
   3.500   0.6286   0.00758   0.00211  -0.0518   0.2342   1.0000
   3.750   0.6529   0.00793   0.00229  -0.0512   0.1972   1.0000
   4.000   0.6775   0.00827   0.00249  -0.0506   0.1656   1.0000
   4.250   0.7025   0.00860   0.00269  -0.0502   0.1384   1.0000
   4.500   0.7275   0.00894   0.00291  -0.0497   0.1137   1.0000
   4.750   0.7526   0.00927   0.00313  -0.0492   0.0930   1.0000
   5.000   0.7780   0.00957   0.00336  -0.0488   0.0768   1.0000
   5.250   0.8031   0.00991   0.00361  -0.0484   0.0593   1.0000
   5.500   0.8281   0.01028   0.00388  -0.0479   0.0446   1.0000
   5.750   0.8539   0.01054   0.00412  -0.0476   0.0395   1.0000
   6.000   0.8795   0.01083   0.00438  -0.0472   0.0355   1.0000
   6.250   0.9055   0.01107   0.00463  -0.0469   0.0339   1.0000
   6.500   0.9313   0.01132   0.00489  -0.0466   0.0327   1.0000
   6.750   0.9569   0.01159   0.00518  -0.0462   0.0314   1.0000
   7.000   0.9822   0.01189   0.00548  -0.0459   0.0299   1.0000
   7.250   1.0071   0.01223   0.00582  -0.0454   0.0284   1.0000
   7.500   1.0319   0.01258   0.00620  -0.0449   0.0270   1.0000
   7.750   1.0573   0.01284   0.00648  -0.0446   0.0265   1.0000
   8.000   1.0824   0.01312   0.00679  -0.0442   0.0258   1.0000
   8.250   1.1073   0.01342   0.00712  -0.0438   0.0250   1.0000
   8.500   1.1319   0.01375   0.00746  -0.0434   0.0240   1.0000
   8.750   1.1560   0.01410   0.00782  -0.0429   0.0228   1.0000
   9.000   1.1795   0.01452   0.00826  -0.0423   0.0216   1.0000
   9.250   1.2029   0.01492   0.00869  -0.0417   0.0208   1.0000
   9.500   1.2271   0.01523   0.00904  -0.0412   0.0201   1.0000
   9.750   1.2509   0.01556   0.00940  -0.0407   0.0191   1.0000
  10.000   1.2741   0.01593   0.00978  -0.0401   0.0178   1.0000
  10.250   1.2966   0.01636   0.01022  -0.0394   0.0165   1.0000
  10.500   1.3188   0.01680   0.01069  -0.0386   0.0155   1.0000
  10.750   1.3406   0.01724   0.01116  -0.0379   0.0144   1.0000
  11.000   1.3617   0.01773   0.01165  -0.0370   0.0130   1.0000
  11.250   1.3820   0.01827   0.01221  -0.0360   0.0118   1.0000
  11.500   1.4018   0.01881   0.01281  -0.0350   0.0110   1.0000
  11.750   1.4205   0.01942   0.01344  -0.0338   0.0101   1.0000
  12.000   1.4380   0.02008   0.01414  -0.0325   0.0093   1.0000
  12.250   1.4549   0.02073   0.01485  -0.0311   0.0088   1.0000
  12.500   1.4696   0.02138   0.01556  -0.0292   0.0084   1.0000
  12.750   1.4829   0.02209   0.01633  -0.0273   0.0081   1.0000
  13.000   1.4950   0.02288   0.01718  -0.0253   0.0077   1.0000
  13.250   1.5061   0.02376   0.01813  -0.0233   0.0073   1.0000
  13.500   1.5158   0.02476   0.01920  -0.0213   0.0070   1.0000
  13.750   1.5240   0.02592   0.02043  -0.0193   0.0066   1.0000
  14.000   1.5336   0.02699   0.02159  -0.0176   0.0065   1.0000
  14.250   1.5423   0.02819   0.02287  -0.0160   0.0063   1.0000
  14.500   1.5499   0.02953   0.02430  -0.0145   0.0061   1.0000
  14.750   1.5565   0.03101   0.02587  -0.0131   0.0059   1.0000
  15.000   1.5618   0.03269   0.02764  -0.0120   0.0058   1.0000
  15.250   1.5660   0.03456   0.02960  -0.0110   0.0056   1.0000
  15.500   1.5688   0.03666   0.03181  -0.0102   0.0054   1.0000
  15.750   1.5701   0.03906   0.03430  -0.0096   0.0053   1.0000
  16.000   1.5696   0.04175   0.03709  -0.0094   0.0052   1.0000
  16.250   1.5673   0.04480   0.04025  -0.0094   0.0050   1.0000
  16.500   1.5628   0.04827   0.04384  -0.0098   0.0049   1.0000
  16.750   1.5557   0.05222   0.04791  -0.0106   0.0048   1.0000
  17.000   1.5460   0.05670   0.05253  -0.0118   0.0048   1.0000
  17.250   1.5377   0.06116   0.05711  -0.0132   0.0047   1.0000
  17.500   1.5267   0.06616   0.06224  -0.0150   0.0047   1.0000
  17.750   1.5136   0.07167   0.06789  -0.0171   0.0047   1.0000
  18.000   1.4975   0.07781   0.07416  -0.0196   0.0046   1.0000
  18.250   1.4790   0.08449   0.08098  -0.0225   0.0046   1.0000
  18.500   1.4576   0.09188   0.08852  -0.0259   0.0046   1.0000
  18.750   1.4323   0.10014   0.09692  -0.0298   0.0046   1.0000
  19.000   1.4054   0.10896   0.10590  -0.0341   0.0046   1.0000
  19.250   1.3745   0.11881   0.11590  -0.0390   0.0046   1.0000
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