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NACA 2410 (naca2410-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 2410 (naca2410-il)
Reynolds number: 500,000
Max Cl/Cd: 75.39 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca2410-il-500000-n5.txt
Download as CSV file: xf-naca2410-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.8770   0.08888   0.08623  -0.0213   1.0000   0.0099
 -14.000  -1.0205   0.05664   0.05364  -0.0426   1.0000   0.0089
 -13.750  -1.0662   0.04080   0.03737  -0.0592   1.0000   0.0087
 -13.500  -1.0787   0.03671   0.03307  -0.0610   1.0000   0.0088
 -13.250  -1.0827   0.03421   0.03041  -0.0600   1.0000   0.0089
 -13.000  -1.0776   0.03214   0.02817  -0.0593   1.0000   0.0091
 -12.750  -1.0687   0.03035   0.02622  -0.0584   1.0000   0.0093
 -12.500  -1.0573   0.02875   0.02445  -0.0575   1.0000   0.0096
 -12.250  -1.0441   0.02730   0.02282  -0.0566   1.0000   0.0098
 -12.000  -1.0293   0.02598   0.02135  -0.0556   1.0000   0.0102
 -11.750  -1.0134   0.02479   0.01999  -0.0545   1.0000   0.0105
 -11.500  -0.9965   0.02372   0.01877  -0.0534   1.0000   0.0108
 -11.250  -0.9810   0.02252   0.01746  -0.0522   1.0000   0.0113
 -11.000  -0.9631   0.02164   0.01649  -0.0510   1.0000   0.0118
 -10.750  -0.9445   0.02087   0.01562  -0.0499   1.0000   0.0123
 -10.500  -0.9256   0.02011   0.01474  -0.0487   1.0000   0.0129
 -10.250  -0.9067   0.01937   0.01389  -0.0474   1.0000   0.0134
 -10.000  -0.8874   0.01867   0.01308  -0.0462   1.0000   0.0140
  -9.750  -0.8684   0.01796   0.01228  -0.0449   1.0000   0.0147
  -9.500  -0.8482   0.01744   0.01172  -0.0437   1.0000   0.0156
  -9.250  -0.8275   0.01700   0.01124  -0.0426   1.0000   0.0166
  -9.000  -0.8052   0.01653   0.01068  -0.0418   0.9998   0.0176
  -8.750  -0.7743   0.01596   0.01003  -0.0428   0.9980   0.0188
  -8.500  -0.7428   0.01554   0.00959  -0.0439   0.9961   0.0202
  -8.250  -0.7105   0.01517   0.00915  -0.0451   0.9945   0.0217
  -8.000  -0.6795   0.01480   0.00871  -0.0460   0.9922   0.0232
  -7.750  -0.6485   0.01433   0.00817  -0.0469   0.9897   0.0246
  -7.500  -0.6164   0.01395   0.00778  -0.0481   0.9875   0.0262
  -7.250  -0.5833   0.01362   0.00739  -0.0494   0.9857   0.0278
  -7.000  -0.5512   0.01330   0.00701  -0.0504   0.9832   0.0293
  -6.750  -0.5197   0.01299   0.00663  -0.0513   0.9797   0.0304
  -6.500  -0.4876   0.01242   0.00603  -0.0525   0.9766   0.0324
  -6.250  -0.4541   0.01206   0.00565  -0.0538   0.9736   0.0341
  -6.000  -0.4252   0.01175   0.00531  -0.0540   0.9674   0.0357
  -5.750  -0.3934   0.01144   0.00495  -0.0549   0.9631   0.0371
  -5.500  -0.3640   0.01118   0.00463  -0.0552   0.9575   0.0381
  -5.250  -0.3348   0.01077   0.00420  -0.0556   0.9513   0.0405
  -5.000  -0.3052   0.01046   0.00388  -0.0559   0.9455   0.0426
  -4.750  -0.2770   0.01021   0.00360  -0.0559   0.9378   0.0447
  -4.500  -0.2480   0.00999   0.00334  -0.0561   0.9309   0.0471
  -4.250  -0.2204   0.00973   0.00308  -0.0560   0.9219   0.0519
  -4.000  -0.1925   0.00951   0.00286  -0.0559   0.9130   0.0581
  -3.750  -0.1649   0.00928   0.00265  -0.0557   0.9031   0.0694
  -3.500  -0.1377   0.00907   0.00246  -0.0555   0.8922   0.0836
  -3.250  -0.1104   0.00888   0.00229  -0.0553   0.8810   0.0987
  -3.000  -0.0832   0.00869   0.00213  -0.0551   0.8689   0.1161
  -2.750  -0.0560   0.00852   0.00199  -0.0548   0.8561   0.1360
  -2.500  -0.0290   0.00836   0.00186  -0.0546   0.8422   0.1595
  -2.000   0.0251   0.00806   0.00165  -0.0541   0.8125   0.2177
  -1.750   0.0520   0.00789   0.00157  -0.0539   0.7967   0.2564
  -1.500   0.0789   0.00774   0.00150  -0.0537   0.7803   0.2975
  -1.250   0.1057   0.00761   0.00144  -0.0535   0.7632   0.3394
  -1.000   0.1323   0.00742   0.00139  -0.0532   0.7457   0.3962
  -0.750   0.1587   0.00725   0.00135  -0.0529   0.7279   0.4590
  -0.500   0.1850   0.00709   0.00134  -0.0526   0.7099   0.5228
  -0.250   0.2109   0.00692   0.00134  -0.0521   0.6917   0.5975
   0.000   0.2364   0.00677   0.00136  -0.0516   0.6737   0.6707
   0.250   0.2617   0.00664   0.00139  -0.0509   0.6555   0.7347
   0.500   0.2866   0.00655   0.00144  -0.0500   0.6371   0.7945
   0.750   0.3108   0.00650   0.00150  -0.0489   0.6189   0.8520
   1.000   0.3358   0.00652   0.00157  -0.0479   0.6005   0.9035
   1.250   0.3664   0.00661   0.00163  -0.0482   0.5815   0.9435
   1.500   0.4015   0.00673   0.00168  -0.0497   0.5618   0.9681
   1.750   0.4365   0.00687   0.00174  -0.0512   0.5426   0.9845
   2.000   0.4724   0.00702   0.00180  -0.0530   0.5233   0.9951
   2.250   0.5046   0.00717   0.00187  -0.0540   0.5048   1.0000
   2.500   0.5297   0.00733   0.00195  -0.0535   0.4838   1.0000
   2.750   0.5539   0.00757   0.00204  -0.0527   0.4512   1.0000
   3.000   0.5785   0.00781   0.00214  -0.0521   0.4201   1.0000
   3.250   0.6033   0.00804   0.00226  -0.0515   0.3921   1.0000
   3.500   0.6280   0.00833   0.00240  -0.0509   0.3593   1.0000
   3.750   0.6523   0.00867   0.00257  -0.0503   0.3214   1.0000
   4.000   0.6765   0.00904   0.00277  -0.0497   0.2817   1.0000
   4.250   0.7004   0.00947   0.00301  -0.0491   0.2396   1.0000
   4.500   0.7246   0.00989   0.00326  -0.0486   0.2046   1.0000
   4.750   0.7488   0.01031   0.00353  -0.0480   0.1710   1.0000
   5.000   0.7729   0.01075   0.00383  -0.0475   0.1397   1.0000
   5.250   0.7970   0.01119   0.00414  -0.0469   0.1126   1.0000
   5.500   0.8212   0.01164   0.00446  -0.0464   0.0905   1.0000
   5.750   0.8455   0.01206   0.00480  -0.0458   0.0718   1.0000
   6.000   0.8694   0.01252   0.00517  -0.0452   0.0554   1.0000
   6.250   0.8938   0.01291   0.00553  -0.0447   0.0471   1.0000
   6.500   0.9184   0.01328   0.00590  -0.0442   0.0426   1.0000
   6.750   0.9431   0.01364   0.00628  -0.0437   0.0401   1.0000
   7.000   0.9674   0.01403   0.00669  -0.0432   0.0379   1.0000
   7.250   0.9909   0.01450   0.00716  -0.0425   0.0356   1.0000
   7.500   1.0147   0.01493   0.00764  -0.0419   0.0342   1.0000
   7.750   1.0386   0.01532   0.00808  -0.0413   0.0332   1.0000
   8.000   1.0622   0.01573   0.00855  -0.0407   0.0319   1.0000
   8.250   1.0854   0.01618   0.00903  -0.0400   0.0305   1.0000
   8.500   1.1078   0.01668   0.00955  -0.0393   0.0291   1.0000
   8.750   1.1286   0.01733   0.01024  -0.0383   0.0276   1.0000
   9.000   1.1504   0.01785   0.01083  -0.0375   0.0266   1.0000
   9.250   1.1729   0.01829   0.01134  -0.0368   0.0257   1.0000
   9.500   1.1947   0.01877   0.01188  -0.0360   0.0246   1.0000
   9.750   1.2162   0.01926   0.01241  -0.0352   0.0234   1.0000
  10.000   1.2367   0.01981   0.01299  -0.0342   0.0222   1.0000
  10.250   1.2543   0.02060   0.01381  -0.0329   0.0209   1.0000
  10.500   1.2749   0.02108   0.01439  -0.0320   0.0202   1.0000
  10.750   1.2945   0.02161   0.01501  -0.0309   0.0191   1.0000
  11.000   1.3136   0.02216   0.01561  -0.0298   0.0179   1.0000
  11.250   1.3318   0.02273   0.01621  -0.0286   0.0167   1.0000
  11.500   1.3460   0.02346   0.01698  -0.0268   0.0158   1.0000
  11.750   1.3598   0.02419   0.01781  -0.0250   0.0150   1.0000
  12.000   1.3731   0.02497   0.01868  -0.0232   0.0142   1.0000
  12.250   1.3858   0.02581   0.01958  -0.0215   0.0134   1.0000
  12.500   1.3975   0.02674   0.02056  -0.0198   0.0127   1.0000
  12.750   1.4064   0.02790   0.02179  -0.0180   0.0120   1.0000
  13.000   1.4155   0.02909   0.02309  -0.0163   0.0115   1.0000
  13.250   1.4237   0.03040   0.02451  -0.0147   0.0110   1.0000
  13.500   1.4313   0.03182   0.02603  -0.0133   0.0105   1.0000
  13.750   1.4376   0.03340   0.02770  -0.0121   0.0101   1.0000
  14.000   1.4425   0.03521   0.02961  -0.0110   0.0097   1.0000
  14.250   1.4450   0.03734   0.03185  -0.0101   0.0093   1.0000
  14.500   1.4442   0.03994   0.03456  -0.0094   0.0090   1.0000
  14.750   1.4453   0.04249   0.03725  -0.0091   0.0089   1.0000
  15.000   1.4447   0.04535   0.04025  -0.0091   0.0087   1.0000
  15.250   1.4425   0.04856   0.04361  -0.0094   0.0085   1.0000
  15.500   1.4385   0.05212   0.04731  -0.0100   0.0083   1.0000
  15.750   1.4330   0.05605   0.05138  -0.0110   0.0082   1.0000
  16.000   1.4255   0.06040   0.05588  -0.0123   0.0081   1.0000
  16.250   1.4162   0.06515   0.06078  -0.0139   0.0079   1.0000
  16.500   1.4050   0.07039   0.06617  -0.0160   0.0078   1.0000
  16.750   1.3918   0.07612   0.07204  -0.0184   0.0078   1.0000
  17.000   1.3766   0.08235   0.07842  -0.0211   0.0077   1.0000
  17.250   1.3597   0.08908   0.08530  -0.0242   0.0076   1.0000
  17.500   1.3405   0.09639   0.09276  -0.0276   0.0076   1.0000
  17.750   1.3197   0.10421   0.10073  -0.0314   0.0076   1.0000
  18.000   1.2974   0.11258   0.10924  -0.0356   0.0076   1.0000
  18.250   1.2740   0.12134   0.11816  -0.0401   0.0076   1.0000
  18.500   1.2497   0.13059   0.12755  -0.0450   0.0076   1.0000
  18.750   1.2246   0.14037   0.13747  -0.0503   0.0077   1.0000
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