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NACA 2410 (naca2410-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 2410 (naca2410-il)
Reynolds number: 500,000
Max Cl/Cd: 86.33 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca2410-il-500000.txt
Download as CSV file: xf-naca2410-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.9101   0.04637   0.04339  -0.0565   1.0000   0.0145
 -12.250  -0.9304   0.04070   0.03747  -0.0607   1.0000   0.0145
 -12.000  -0.9458   0.03698   0.03350  -0.0599   1.0000   0.0146
 -11.750  -0.9454   0.03434   0.03068  -0.0591   1.0000   0.0149
 -11.500  -0.9352   0.03280   0.02903  -0.0582   1.0000   0.0152
 -11.250  -0.9218   0.03159   0.02772  -0.0573   1.0000   0.0156
 -11.000  -0.9078   0.03041   0.02642  -0.0562   1.0000   0.0161
 -10.750  -0.8947   0.02904   0.02487  -0.0550   1.0000   0.0168
 -10.500  -0.8820   0.02758   0.02321  -0.0535   1.0000   0.0174
 -10.250  -0.8684   0.02620   0.02161  -0.0519   1.0000   0.0180
 -10.000  -0.8559   0.02453   0.01967  -0.0501   1.0000   0.0185
  -9.750  -0.8444   0.02265   0.01763  -0.0482   1.0000   0.0194
  -9.500  -0.8258   0.02212   0.01707  -0.0469   1.0000   0.0201
  -9.250  -0.8070   0.02159   0.01648  -0.0455   1.0000   0.0210
  -9.000  -0.7886   0.02092   0.01568  -0.0440   1.0000   0.0220
  -8.750  -0.7694   0.02041   0.01504  -0.0426   1.0000   0.0231
  -8.500  -0.7529   0.01913   0.01357  -0.0410   1.0000   0.0244
  -8.250  -0.7341   0.01849   0.01292  -0.0397   1.0000   0.0256
  -8.000  -0.7141   0.01811   0.01251  -0.0384   1.0000   0.0269
  -7.750  -0.6938   0.01766   0.01196  -0.0372   1.0000   0.0285
  -7.500  -0.6728   0.01743   0.01164  -0.0360   1.0000   0.0298
  -7.250  -0.6539   0.01613   0.01022  -0.0348   1.0000   0.0320
  -7.000  -0.6274   0.01573   0.00983  -0.0349   0.9993   0.0339
  -6.750  -0.5916   0.01531   0.00933  -0.0367   0.9972   0.0362
  -6.500  -0.5541   0.01513   0.00905  -0.0388   0.9952   0.0380
  -6.250  -0.5209   0.01382   0.00768  -0.0405   0.9931   0.0410
  -6.000  -0.4857   0.01341   0.00726  -0.0422   0.9901   0.0435
  -5.750  -0.4494   0.01302   0.00681  -0.0441   0.9877   0.0458
  -5.500  -0.4122   0.01271   0.00644  -0.0461   0.9857   0.0475
  -5.250  -0.3787   0.01188   0.00557  -0.0476   0.9829   0.0504
  -5.000  -0.3446   0.01145   0.00514  -0.0490   0.9793   0.0532
  -4.750  -0.3081   0.01110   0.00475  -0.0509   0.9768   0.0562
  -4.500  -0.2701   0.01078   0.00439  -0.0530   0.9750   0.0587
  -4.250  -0.2354   0.01026   0.00391  -0.0545   0.9717   0.0659
  -4.000  -0.2022   0.00987   0.00356  -0.0556   0.9671   0.0772
  -3.750  -0.1676   0.00940   0.00324  -0.0571   0.9636   0.1062
  -3.500  -0.1361   0.00905   0.00301  -0.0579   0.9584   0.1389
  -3.250  -0.1061   0.00874   0.00281  -0.0583   0.9518   0.1704
  -3.000  -0.0757   0.00844   0.00263  -0.0588   0.9458   0.2045
  -2.750  -0.0485   0.00816   0.00247  -0.0585   0.9369   0.2410
  -2.500  -0.0208   0.00788   0.00233  -0.0584   0.9284   0.2831
  -2.250   0.0061   0.00760   0.00219  -0.0581   0.9190   0.3296
  -2.000   0.0322   0.00731   0.00208  -0.0576   0.9078   0.3854
  -1.750   0.0580   0.00695   0.00197  -0.0571   0.8968   0.4657
  -1.500   0.0832   0.00657   0.00190  -0.0564   0.8852   0.5614
  -1.250   0.1081   0.00626   0.00185  -0.0556   0.8723   0.6473
  -1.000   0.1322   0.00598   0.00182  -0.0545   0.8583   0.7317
  -0.750   0.1560   0.00577   0.00182  -0.0531   0.8437   0.8054
  -0.500   0.1796   0.00565   0.00182  -0.0517   0.8285   0.8664
  -0.250   0.2051   0.00562   0.00184  -0.0505   0.8127   0.9203
   0.000   0.2385   0.00568   0.00185  -0.0512   0.7963   0.9579
   0.250   0.2767   0.00575   0.00184  -0.0531   0.7785   0.9778
   0.500   0.3175   0.00583   0.00183  -0.0558   0.7591   0.9899
   0.750   0.3600   0.00592   0.00182  -0.0589   0.7385   0.9985
   1.000   0.3884   0.00602   0.00180  -0.0590   0.7175   1.0000
   1.250   0.4134   0.00611   0.00180  -0.0584   0.6958   1.0000
   1.500   0.4383   0.00623   0.00181  -0.0577   0.6748   1.0000
   1.750   0.4633   0.00635   0.00183  -0.0570   0.6535   1.0000
   2.000   0.4883   0.00649   0.00188  -0.0564   0.6323   1.0000
   2.250   0.5131   0.00664   0.00193  -0.0557   0.6119   1.0000
   2.500   0.5379   0.00679   0.00199  -0.0550   0.5885   1.0000
   2.750   0.5622   0.00699   0.00207  -0.0542   0.5605   1.0000
   3.000   0.5868   0.00719   0.00216  -0.0535   0.5357   1.0000
   3.250   0.6120   0.00737   0.00226  -0.0529   0.5128   1.0000
   3.500   0.6370   0.00758   0.00238  -0.0523   0.4889   1.0000
   3.750   0.6621   0.00779   0.00250  -0.0518   0.4631   1.0000
   4.000   0.6873   0.00802   0.00263  -0.0512   0.4363   1.0000
   4.250   0.7124   0.00827   0.00279  -0.0507   0.4084   1.0000
   4.500   0.7373   0.00854   0.00297  -0.0502   0.3792   1.0000
   4.750   0.7620   0.00887   0.00316  -0.0496   0.3453   1.0000
   5.000   0.7861   0.00927   0.00340  -0.0490   0.3059   1.0000
   5.250   0.8095   0.00976   0.00369  -0.0483   0.2602   1.0000
   5.500   0.8323   0.01034   0.00403  -0.0476   0.2103   1.0000
   5.750   0.8542   0.01103   0.00446  -0.0468   0.1580   1.0000
   6.000   0.8754   0.01183   0.00495  -0.0459   0.1058   1.0000
   6.250   0.8969   0.01259   0.00550  -0.0449   0.0705   1.0000
   6.500   0.9200   0.01316   0.00600  -0.0442   0.0586   1.0000
   6.750   0.9431   0.01372   0.00658  -0.0434   0.0532   1.0000
   7.000   0.9672   0.01414   0.00704  -0.0427   0.0503   1.0000
   7.250   0.9905   0.01464   0.00755  -0.0420   0.0477   1.0000
   7.500   1.0119   0.01533   0.00826  -0.0410   0.0450   1.0000
   7.750   1.0332   0.01601   0.00901  -0.0400   0.0432   1.0000
   8.000   1.0563   0.01647   0.00954  -0.0393   0.0418   1.0000
   8.250   1.0787   0.01699   0.01011  -0.0385   0.0401   1.0000
   8.500   1.1005   0.01755   0.01071  -0.0376   0.0383   1.0000
   8.750   1.1201   0.01832   0.01150  -0.0365   0.0364   1.0000
   9.000   1.1350   0.01962   0.01287  -0.0346   0.0345   1.0000
   9.250   1.1572   0.02005   0.01339  -0.0339   0.0334   1.0000
   9.500   1.1783   0.02060   0.01401  -0.0329   0.0318   1.0000
   9.750   1.1984   0.02117   0.01463  -0.0320   0.0301   1.0000
  10.000   1.2159   0.02199   0.01546  -0.0307   0.0285   1.0000
  10.250   1.2265   0.02368   0.01724  -0.0284   0.0269   1.0000
  10.500   1.2464   0.02410   0.01777  -0.0274   0.0257   1.0000
  10.750   1.2639   0.02469   0.01845  -0.0261   0.0243   1.0000
  11.000   1.2791   0.02528   0.01908  -0.0244   0.0230   1.0000
  11.250   1.2912   0.02613   0.01995  -0.0225   0.0219   1.0000
  11.500   1.2951   0.02802   0.02194  -0.0197   0.0208   1.0000
  11.750   1.3087   0.02875   0.02279  -0.0181   0.0200   1.0000
  12.000   1.3200   0.02975   0.02391  -0.0164   0.0191   1.0000
  12.250   1.3306   0.03078   0.02505  -0.0148   0.0183   1.0000
  12.500   1.3411   0.03180   0.02612  -0.0134   0.0175   1.0000
  12.750   1.3500   0.03302   0.02738  -0.0121   0.0169   1.0000
  13.000   1.3490   0.03537   0.02982  -0.0102   0.0162   1.0000
  13.250   1.3528   0.03733   0.03194  -0.0090   0.0157   1.0000
  13.500   1.3584   0.03914   0.03390  -0.0081   0.0152   1.0000
  13.750   1.3616   0.04132   0.03622  -0.0074   0.0148   1.0000
  14.000   1.3633   0.04372   0.03877  -0.0069   0.0143   1.0000
  14.250   1.3644   0.04632   0.04149  -0.0067   0.0140   1.0000
  14.500   1.3646   0.04913   0.04441  -0.0068   0.0136   1.0000
  14.750   1.3641   0.05213   0.04753  -0.0073   0.0133   1.0000
  15.000   1.3620   0.05548   0.05098  -0.0080   0.0131   1.0000
  15.250   1.3572   0.05930   0.05492  -0.0090   0.0129   1.0000
  15.500   1.3488   0.06374   0.05949  -0.0104   0.0127   1.0000
  15.750   1.3362   0.06895   0.06484  -0.0121   0.0125   1.0000
  16.000   1.3202   0.07486   0.07092  -0.0143   0.0123   1.0000
  16.250   1.3009   0.08158   0.07782  -0.0170   0.0122   1.0000
  16.500   1.2801   0.08889   0.08532  -0.0203   0.0122   1.0000
  17.000   1.2385   0.10461   0.10139  -0.0284   0.0121   1.0000
  17.250   1.2175   0.11304   0.10999  -0.0330   0.0121   1.0000
  17.500   1.1951   0.12212   0.11924  -0.0381   0.0121   1.0000
  17.750   1.1742   0.13137   0.12864  -0.0435   0.0122   1.0000
  18.000   1.1536   0.14101   0.13841  -0.0492   0.0123   1.0000
  18.250   1.1250   0.15325   0.15083  -0.0565   0.0124   1.0000
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