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NACA 2410 (naca2410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 2410 (naca2410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.47 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca2410-il-1000000.txt
Download as CSV file: xf-naca2410-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -1.0113   0.07601   0.07376  -0.0290   1.0000   0.0088
 -14.750  -1.0707   0.06077   0.05831  -0.0388   1.0000   0.0084
 -14.500  -1.0990   0.04855   0.04588  -0.0492   1.0000   0.0083
 -14.250  -1.1169   0.03930   0.03639  -0.0596   1.0000   0.0082
 -14.000  -1.1355   0.03436   0.03122  -0.0623   1.0000   0.0083
 -13.750  -1.1483   0.03120   0.02784  -0.0608   1.0000   0.0084
 -13.500  -1.1470   0.02874   0.02521  -0.0597   1.0000   0.0086
 -13.250  -1.1370   0.02706   0.02341  -0.0587   1.0000   0.0089
 -13.000  -1.1225   0.02580   0.02205  -0.0579   1.0000   0.0091
 -12.750  -1.1061   0.02473   0.02088  -0.0570   1.0000   0.0094
 -12.500  -1.0891   0.02369   0.01974  -0.0562   1.0000   0.0096
 -12.250  -1.0717   0.02270   0.01864  -0.0552   1.0000   0.0099
 -12.000  -1.0542   0.02174   0.01756  -0.0541   1.0000   0.0102
 -11.750  -1.0364   0.02087   0.01657  -0.0529   1.0000   0.0105
 -11.500  -1.0177   0.02013   0.01573  -0.0517   1.0000   0.0107
 -11.250  -1.0026   0.01894   0.01438  -0.0501   1.0000   0.0110
 -11.000  -0.9873   0.01780   0.01313  -0.0484   1.0000   0.0117
 -10.750  -0.9684   0.01713   0.01241  -0.0471   1.0000   0.0122
 -10.500  -0.9489   0.01659   0.01181  -0.0458   1.0000   0.0126
 -10.250  -0.9292   0.01607   0.01122  -0.0444   1.0000   0.0132
 -10.000  -0.9092   0.01560   0.01068  -0.0431   1.0000   0.0137
  -9.750  -0.8885   0.01525   0.01026  -0.0419   1.0000   0.0141
  -9.500  -0.8707   0.01438   0.00932  -0.0403   1.0000   0.0154
  -9.250  -0.8497   0.01404   0.00898  -0.0392   1.0000   0.0164
  -9.000  -0.8227   0.01373   0.00863  -0.0393   0.9995   0.0174
  -8.750  -0.7897   0.01344   0.00829  -0.0405   0.9983   0.0183
  -8.500  -0.7577   0.01282   0.00765  -0.0417   0.9970   0.0202
  -8.250  -0.7238   0.01265   0.00748  -0.0432   0.9958   0.0218
  -8.000  -0.6892   0.01253   0.00735  -0.0447   0.9948   0.0232
  -7.750  -0.6567   0.01203   0.00679  -0.0459   0.9934   0.0250
  -7.500  -0.6240   0.01175   0.00652  -0.0471   0.9913   0.0267
  -7.250  -0.5896   0.01153   0.00629  -0.0486   0.9893   0.0283
  -7.000  -0.5542   0.01138   0.00611  -0.0503   0.9877   0.0297
  -6.750  -0.5195   0.01093   0.00561  -0.0519   0.9863   0.0312
  -6.500  -0.4850   0.01042   0.00509  -0.0535   0.9852   0.0334
  -6.250  -0.4522   0.01016   0.00483  -0.0547   0.9829   0.0351
  -6.000  -0.4204   0.00991   0.00455  -0.0555   0.9797   0.0365
  -5.750  -0.3876   0.00968   0.00430  -0.0566   0.9770   0.0376
  -5.500  -0.3551   0.00940   0.00398  -0.0576   0.9744   0.0386
  -5.250  -0.3277   0.00896   0.00350  -0.0575   0.9687   0.0410
  -5.000  -0.2986   0.00868   0.00321  -0.0577   0.9637   0.0430
  -4.750  -0.2708   0.00846   0.00297  -0.0576   0.9576   0.0450
  -4.500  -0.2435   0.00826   0.00275  -0.0573   0.9506   0.0467
  -4.250  -0.2163   0.00806   0.00251  -0.0570   0.9433   0.0492
  -4.000  -0.1895   0.00781   0.00228  -0.0566   0.9351   0.0557
  -3.750  -0.1627   0.00756   0.00208  -0.0563   0.9264   0.0701
  -3.500  -0.1361   0.00730   0.00190  -0.0560   0.9174   0.0952
  -3.250  -0.1091   0.00710   0.00176  -0.0557   0.9070   0.1166
  -3.000  -0.0820   0.00692   0.00164  -0.0554   0.8967   0.1398
  -2.750  -0.0550   0.00675   0.00152  -0.0552   0.8856   0.1649
  -2.500  -0.0278   0.00659   0.00142  -0.0550   0.8732   0.1923
  -2.250  -0.0006   0.00643   0.00133  -0.0548   0.8603   0.2226
  -2.000   0.0267   0.00629   0.00125  -0.0546   0.8466   0.2560
  -1.750   0.0539   0.00616   0.00118  -0.0544   0.8322   0.2923
  -1.500   0.0810   0.00600   0.00112  -0.0542   0.8169   0.3389
  -1.250   0.1077   0.00578   0.00107  -0.0540   0.8008   0.4051
  -1.000   0.1344   0.00558   0.00103  -0.0538   0.7841   0.4750
  -0.750   0.1610   0.00541   0.00101  -0.0535   0.7669   0.5452
  -0.500   0.1874   0.00523   0.00100  -0.0532   0.7492   0.6212
  -0.250   0.2133   0.00504   0.00102  -0.0527   0.7308   0.7045
   0.000   0.2392   0.00493   0.00103  -0.0521   0.7117   0.7654
   0.250   0.2641   0.00482   0.00107  -0.0512   0.6922   0.8319
   0.500   0.2876   0.00476   0.00113  -0.0499   0.6727   0.8963
   0.750   0.3127   0.00479   0.00118  -0.0490   0.6524   0.9398
   1.000   0.3433   0.00489   0.00122  -0.0494   0.6316   0.9661
   1.250   0.3777   0.00501   0.00126  -0.0507   0.6108   0.9815
   1.500   0.4143   0.00514   0.00130  -0.0526   0.5891   0.9908
   2.000   0.4881   0.00546   0.00141  -0.0566   0.5404   1.0000
   2.250   0.5127   0.00565   0.00146  -0.0560   0.5093   1.0000
   2.500   0.5377   0.00580   0.00152  -0.0554   0.4854   1.0000
   2.750   0.5629   0.00596   0.00159  -0.0548   0.4640   1.0000
   3.000   0.5883   0.00611   0.00166  -0.0543   0.4456   1.0000
   3.250   0.6135   0.00628   0.00175  -0.0537   0.4217   1.0000
   3.500   0.6386   0.00649   0.00186  -0.0532   0.3949   1.0000
   3.750   0.6637   0.00674   0.00198  -0.0527   0.3654   1.0000
   4.000   0.6888   0.00700   0.00211  -0.0522   0.3350   1.0000
   4.250   0.7138   0.00730   0.00228  -0.0516   0.3009   1.0000
   4.500   0.7383   0.00767   0.00248  -0.0511   0.2622   1.0000
   4.750   0.7625   0.00810   0.00271  -0.0505   0.2206   1.0000
   5.000   0.7865   0.00856   0.00297  -0.0499   0.1792   1.0000
   5.250   0.8102   0.00907   0.00328  -0.0493   0.1372   1.0000
   5.500   0.8339   0.00958   0.00360  -0.0487   0.1010   1.0000
   5.750   0.8575   0.01011   0.00396  -0.0480   0.0694   1.0000
   6.000   0.8816   0.01059   0.00431  -0.0475   0.0500   1.0000
   6.250   0.9065   0.01098   0.00466  -0.0469   0.0432   1.0000
   6.500   0.9321   0.01126   0.00496  -0.0466   0.0413   1.0000
   6.750   0.9573   0.01159   0.00530  -0.0461   0.0391   1.0000
   7.000   0.9820   0.01197   0.00569  -0.0456   0.0369   1.0000
   7.250   1.0056   0.01249   0.00625  -0.0449   0.0347   1.0000
   7.500   1.0310   0.01275   0.00654  -0.0446   0.0341   1.0000
   7.750   1.0560   0.01305   0.00688  -0.0441   0.0332   1.0000
   8.000   1.0807   0.01339   0.00724  -0.0437   0.0320   1.0000
   8.250   1.1050   0.01375   0.00764  -0.0432   0.0309   1.0000
   8.500   1.1285   0.01419   0.00808  -0.0426   0.0294   1.0000
   8.750   1.1489   0.01494   0.00889  -0.0415   0.0275   1.0000
   9.000   1.1721   0.01537   0.00937  -0.0408   0.0268   1.0000
   9.250   1.1967   0.01564   0.00967  -0.0404   0.0260   1.0000
   9.500   1.2207   0.01594   0.01000  -0.0399   0.0249   1.0000
   9.750   1.2445   0.01626   0.01033  -0.0394   0.0236   1.0000
  10.000   1.2667   0.01673   0.01079  -0.0387   0.0223   1.0000
  10.250   1.2852   0.01751   0.01165  -0.0374   0.0208   1.0000
  10.500   1.3095   0.01773   0.01189  -0.0370   0.0200   1.0000
  10.750   1.3328   0.01803   0.01222  -0.0364   0.0188   1.0000
  11.000   1.3554   0.01836   0.01254  -0.0358   0.0175   1.0000
  11.250   1.3730   0.01911   0.01331  -0.0344   0.0159   1.0000
  11.500   1.3946   0.01948   0.01373  -0.0336   0.0151   1.0000
  11.750   1.4146   0.01995   0.01423  -0.0326   0.0141   1.0000
  12.000   1.4328   0.02055   0.01483  -0.0314   0.0132   1.0000
  12.250   1.4429   0.02158   0.01592  -0.0290   0.0121   1.0000
  12.500   1.4575   0.02221   0.01662  -0.0272   0.0117   1.0000
  12.750   1.4704   0.02295   0.01744  -0.0252   0.0112   1.0000
  13.000   1.4825   0.02377   0.01832  -0.0233   0.0107   1.0000
  13.250   1.4932   0.02470   0.01932  -0.0214   0.0103   1.0000
  13.500   1.5013   0.02585   0.02053  -0.0194   0.0098   1.0000
  13.750   1.5035   0.02749   0.02227  -0.0169   0.0093   1.0000
  14.000   1.5049   0.02929   0.02419  -0.0148   0.0090   1.0000
  14.250   1.5134   0.03061   0.02561  -0.0135   0.0088   1.0000
  14.500   1.5198   0.03217   0.02727  -0.0123   0.0086   1.0000
  14.750   1.5250   0.03394   0.02913  -0.0112   0.0083   1.0000
  15.000   1.5283   0.03597   0.03126  -0.0104   0.0081   1.0000
  15.250   1.5302   0.03827   0.03367  -0.0098   0.0079   1.0000
  15.500   1.5309   0.04083   0.03634  -0.0094   0.0078   1.0000
  15.750   1.5297   0.04373   0.03935  -0.0094   0.0076   1.0000
  16.000   1.5263   0.04707   0.04280  -0.0097   0.0075   1.0000
  16.250   1.5205   0.05084   0.04669  -0.0104   0.0073   1.0000
  16.500   1.5117   0.05520   0.05117  -0.0116   0.0072   1.0000
  16.750   1.4997   0.06019   0.05630  -0.0132   0.0071   1.0000
  17.000   1.4850   0.06578   0.06202  -0.0152   0.0071   1.0000
  17.250   1.4668   0.07214   0.06853  -0.0177   0.0070   1.0000
  17.500   1.4479   0.07880   0.07533  -0.0205   0.0069   1.0000
  17.750   1.4265   0.08610   0.08277  -0.0238   0.0069   1.0000
  18.000   1.4057   0.09351   0.09032  -0.0271   0.0069   1.0000
  18.250   1.3828   0.10145   0.09840  -0.0309   0.0069   1.0000
  18.500   1.3608   0.10948   0.10656  -0.0347   0.0069   1.0000
  18.750   1.3376   0.11792   0.11513  -0.0389   0.0069   1.0000
  19.000   1.3150   0.12641   0.12374  -0.0432   0.0069   1.0000
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