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NACA 0010 (naca0010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0010 (naca0010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.15 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca0010-il-1000000.txt
Download as CSV file: xf-naca0010-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.0039   0.15161   0.14975   0.0348   1.0000   0.0085
 -17.750  -1.0775   0.13031   0.12822   0.0233   1.0000   0.0082
 -17.500  -1.1221   0.11680   0.11455   0.0161   1.0000   0.0080
 -17.250  -1.1624   0.10480   0.10239   0.0099   1.0000   0.0079
 -17.000  -1.1984   0.09402   0.09147   0.0042   1.0000   0.0077
 -16.750  -1.2283   0.08447   0.08177  -0.0008   1.0000   0.0076
 -16.500  -1.2553   0.07551   0.07267  -0.0058   1.0000   0.0076
 -16.250  -1.2801   0.06692   0.06393  -0.0109   1.0000   0.0075
 -16.000  -1.3026   0.05885   0.05569  -0.0160   1.0000   0.0075
 -15.750  -1.3211   0.05178   0.04845  -0.0205   1.0000   0.0075
 -15.500  -1.3399   0.04522   0.04170  -0.0245   1.0000   0.0076
 -15.250  -1.3531   0.04023   0.03653  -0.0269   1.0000   0.0077
 -15.000  -1.3634   0.03627   0.03241  -0.0278   1.0000   0.0078
 -14.750  -1.3685   0.03339   0.02938  -0.0274   1.0000   0.0079
 -14.500  -1.3699   0.03118   0.02706  -0.0263   1.0000   0.0081
 -14.250  -1.3672   0.02949   0.02527  -0.0248   1.0000   0.0083
 -14.000  -1.3617   0.02814   0.02382  -0.0229   1.0000   0.0085
 -13.750  -1.3544   0.02700   0.02259  -0.0209   1.0000   0.0087
 -13.500  -1.3446   0.02599   0.02149  -0.0189   1.0000   0.0090
 -13.250  -1.3310   0.02500   0.02041  -0.0175   1.0000   0.0092
 -13.000  -1.3156   0.02409   0.01940  -0.0163   1.0000   0.0095
 -12.750  -1.2988   0.02324   0.01844  -0.0151   1.0000   0.0098
 -12.500  -1.2804   0.02249   0.01760  -0.0141   1.0000   0.0100
 -12.250  -1.2695   0.02091   0.01586  -0.0123   1.0000   0.0106
 -12.000  -1.2517   0.01997   0.01486  -0.0112   1.0000   0.0112
 -11.750  -1.2312   0.01929   0.01413  -0.0103   1.0000   0.0117
 -11.500  -1.2099   0.01869   0.01347  -0.0096   1.0000   0.0123
 -11.250  -1.1880   0.01811   0.01282  -0.0089   1.0000   0.0129
 -11.000  -1.1652   0.01763   0.01226  -0.0083   1.0000   0.0133
 -10.750  -1.1457   0.01670   0.01127  -0.0072   1.0000   0.0146
 -10.500  -1.1220   0.01629   0.01087  -0.0068   1.0000   0.0157
 -10.250  -1.0975   0.01596   0.01052  -0.0063   1.0000   0.0168
 -10.000  -1.0727   0.01568   0.01020  -0.0059   1.0000   0.0176
  -9.750  -1.0509   0.01498   0.00946  -0.0051   1.0000   0.0192
  -9.500  -1.0259   0.01471   0.00920  -0.0047   1.0000   0.0206
  -9.250  -1.0006   0.01448   0.00896  -0.0044   1.0000   0.0219
  -9.000  -0.9748   0.01434   0.00879  -0.0041   1.0000   0.0229
  -8.750  -0.9515   0.01384   0.00824  -0.0034   1.0000   0.0242
  -8.500  -0.9284   0.01335   0.00775  -0.0027   1.0000   0.0260
  -8.250  -0.9039   0.01307   0.00746  -0.0022   1.0000   0.0272
  -8.000  -0.8794   0.01281   0.00717  -0.0016   1.0000   0.0285
  -7.750  -0.8547   0.01261   0.00695  -0.0010   1.0000   0.0295
  -7.500  -0.8300   0.01245   0.00678  -0.0004   1.0000   0.0301
  -7.250  -0.8094   0.01176   0.00600   0.0009   1.0000   0.0318
  -7.000  -0.7868   0.01134   0.00557   0.0018   1.0000   0.0335
  -6.750  -0.7635   0.01105   0.00527   0.0027   1.0000   0.0349
  -6.500  -0.7402   0.01079   0.00499   0.0036   1.0000   0.0362
  -6.250  -0.7170   0.01054   0.00472   0.0045   1.0000   0.0373
  -6.000  -0.6937   0.01033   0.00448   0.0054   1.0000   0.0381
  -5.750  -0.6706   0.01010   0.00422   0.0063   1.0000   0.0388
  -5.500  -0.6483   0.00974   0.00383   0.0074   1.0000   0.0411
  -5.250  -0.6255   0.00947   0.00357   0.0084   1.0000   0.0438
  -5.000  -0.5967   0.00923   0.00333   0.0081   0.9993   0.0465
  -4.750  -0.5618   0.00893   0.00306   0.0065   0.9975   0.0536
  -4.500  -0.5272   0.00853   0.00280   0.0049   0.9957   0.0772
  -4.250  -0.4920   0.00814   0.00257   0.0031   0.9941   0.1094
  -4.000  -0.4588   0.00779   0.00237   0.0018   0.9911   0.1424
  -3.750  -0.4244   0.00744   0.00219   0.0002   0.9883   0.1787
  -3.500  -0.3888   0.00711   0.00202  -0.0017   0.9861   0.2177
  -3.250  -0.3541   0.00679   0.00187  -0.0033   0.9832   0.2589
  -3.000  -0.3227   0.00650   0.00173  -0.0041   0.9774   0.2987
  -2.750  -0.2908   0.00622   0.00161  -0.0050   0.9716   0.3397
  -2.500  -0.2620   0.00596   0.00150  -0.0052   0.9626   0.3825
  -2.250  -0.2347   0.00572   0.00141  -0.0050   0.9515   0.4241
  -2.000  -0.2080   0.00552   0.00132  -0.0046   0.9390   0.4619
  -1.750  -0.1818   0.00534   0.00124  -0.0041   0.9244   0.5007
  -1.500  -0.1561   0.00515   0.00117  -0.0035   0.9075   0.5463
  -1.250  -0.1303   0.00500   0.00111  -0.0029   0.8884   0.5859
  -1.000  -0.1044   0.00489   0.00106  -0.0023   0.8671   0.6249
  -0.750  -0.0786   0.00478   0.00102  -0.0016   0.8429   0.6658
  -0.500  -0.0524   0.00472   0.00100  -0.0011   0.8166   0.6989
  -0.250  -0.0262   0.00470   0.00098  -0.0005   0.7889   0.7294
   0.000   0.0000   0.00469   0.00097   0.0000   0.7590   0.7592
   0.250   0.0262   0.00470   0.00098   0.0005   0.7291   0.7887
   0.500   0.0525   0.00472   0.00100   0.0011   0.6986   0.8166
   0.750   0.0786   0.00478   0.00102   0.0016   0.6654   0.8428
   1.000   0.1044   0.00489   0.00106   0.0023   0.6248   0.8669
   1.250   0.1304   0.00500   0.00111   0.0029   0.5859   0.8882
   1.500   0.1562   0.00514   0.00117   0.0035   0.5480   0.9074
   1.750   0.1818   0.00534   0.00124   0.0041   0.5004   0.9245
   2.000   0.2080   0.00552   0.00132   0.0046   0.4619   0.9390
   2.250   0.2347   0.00573   0.00141   0.0050   0.4236   0.9515
   2.500   0.2620   0.00596   0.00150   0.0052   0.3823   0.9626
   2.750   0.2908   0.00622   0.00161   0.0050   0.3395   0.9716
   3.000   0.3227   0.00650   0.00173   0.0041   0.2987   0.9774
   3.250   0.3542   0.00679   0.00187   0.0033   0.2590   0.9832
   3.500   0.3888   0.00711   0.00202   0.0017   0.2176   0.9861
   3.750   0.4244   0.00744   0.00219  -0.0002   0.1787   0.9883
   4.000   0.4588   0.00779   0.00237  -0.0018   0.1425   0.9911
   4.250   0.4920   0.00814   0.00257  -0.0031   0.1094   0.9941
   4.500   0.5272   0.00853   0.00280  -0.0049   0.0773   0.9957
   4.750   0.5619   0.00893   0.00306  -0.0065   0.0536   0.9975
   5.000   0.5967   0.00923   0.00333  -0.0081   0.0465   0.9993
   5.250   0.6255   0.00947   0.00357  -0.0084   0.0438   1.0000
   5.500   0.6483   0.00974   0.00383  -0.0074   0.0412   1.0000
   5.750   0.6706   0.01010   0.00422  -0.0063   0.0388   1.0000
   6.000   0.6936   0.01033   0.00448  -0.0054   0.0381   1.0000
   6.250   0.7169   0.01054   0.00472  -0.0045   0.0373   1.0000
   6.500   0.7402   0.01078   0.00499  -0.0036   0.0361   1.0000
   6.750   0.7635   0.01105   0.00527  -0.0027   0.0349   1.0000
   7.000   0.7868   0.01134   0.00557  -0.0018   0.0335   1.0000
   7.250   0.8093   0.01176   0.00600  -0.0009   0.0318   1.0000
   7.500   0.8300   0.01245   0.00677   0.0004   0.0301   1.0000
   7.750   0.8548   0.01260   0.00694   0.0010   0.0295   1.0000
   8.000   0.8794   0.01281   0.00717   0.0016   0.0285   1.0000
   8.250   0.9039   0.01307   0.00746   0.0022   0.0272   1.0000
   8.500   0.9285   0.01335   0.00774   0.0027   0.0260   1.0000
   8.750   0.9516   0.01384   0.00824   0.0034   0.0242   1.0000
   9.000   0.9747   0.01434   0.00880   0.0041   0.0229   1.0000
   9.250   1.0007   0.01448   0.00896   0.0044   0.0219   1.0000
   9.500   1.0260   0.01471   0.00920   0.0047   0.0206   1.0000
   9.750   1.0509   0.01498   0.00946   0.0051   0.0192   1.0000
  10.000   1.0727   0.01568   0.01020   0.0059   0.0176   1.0000
  10.250   1.0975   0.01596   0.01052   0.0063   0.0168   1.0000
  10.500   1.1220   0.01628   0.01087   0.0068   0.0157   1.0000
  10.750   1.1457   0.01669   0.01127   0.0072   0.0146   1.0000
  11.000   1.1652   0.01762   0.01226   0.0083   0.0133   1.0000
  11.250   1.1880   0.01811   0.01282   0.0089   0.0129   1.0000
  11.500   1.2099   0.01868   0.01347   0.0096   0.0123   1.0000
  11.750   1.2313   0.01929   0.01413   0.0103   0.0117   1.0000
  12.000   1.2518   0.01997   0.01487   0.0111   0.0112   1.0000
  12.250   1.2696   0.02091   0.01587   0.0122   0.0106   1.0000
  12.500   1.2807   0.02249   0.01760   0.0141   0.0100   1.0000
  12.750   1.2991   0.02324   0.01844   0.0151   0.0098   1.0000
  13.000   1.3159   0.02409   0.01940   0.0162   0.0095   1.0000
  13.250   1.3311   0.02502   0.02043   0.0175   0.0092   1.0000
  13.500   1.3448   0.02599   0.02150   0.0189   0.0090   1.0000
  13.750   1.3547   0.02701   0.02260   0.0208   0.0087   1.0000
  14.000   1.3622   0.02814   0.02383   0.0228   0.0085   1.0000
  14.250   1.3679   0.02948   0.02525   0.0247   0.0083   1.0000
  14.500   1.3705   0.03117   0.02705   0.0262   0.0081   1.0000
  14.750   1.3695   0.03335   0.02935   0.0273   0.0080   1.0000
  15.000   1.3640   0.03629   0.03242   0.0276   0.0078   1.0000
  15.250   1.3544   0.04017   0.03647   0.0267   0.0077   1.0000
  15.500   1.3403   0.04530   0.04178   0.0243   0.0076   1.0000
  15.750   1.3221   0.05179   0.04846   0.0203   0.0075   1.0000
  16.000   1.3030   0.05898   0.05583   0.0157   0.0075   1.0000
  16.250   1.2811   0.06697   0.06399   0.0106   0.0075   1.0000
  16.500   1.2569   0.07548   0.07265   0.0056   0.0076   1.0000
  16.750   1.2294   0.08456   0.08186   0.0005   0.0076   1.0000
  17.000   1.1991   0.09421   0.09165  -0.0046   0.0077   1.0000
  17.250   1.1635   0.10491   0.10250  -0.0102   0.0079   1.0000
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