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NACA 0010-64 (naca001064-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0010-64 (naca001064-il)
Reynolds number: 1,000,000
Max Cl/Cd: 62.5 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca001064-il-1000000.txt
Download as CSV file: xf-naca001064-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-64                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.1225   0.09487   0.09270  -0.0112   1.0000   0.0094
 -16.750  -1.1644   0.08148   0.07912  -0.0188   1.0000   0.0092
 -16.500  -1.1898   0.07143   0.06890  -0.0254   1.0000   0.0091
 -16.250  -1.2122   0.06267   0.05997  -0.0314   1.0000   0.0090
 -16.000  -1.2353   0.05494   0.05204  -0.0362   1.0000   0.0090
 -15.750  -1.2589   0.04825   0.04514  -0.0395   1.0000   0.0091
 -15.500  -1.2801   0.04285   0.03952  -0.0408   1.0000   0.0092
 -15.250  -1.2964   0.03865   0.03513  -0.0406   1.0000   0.0093
 -15.000  -1.3045   0.03568   0.03201  -0.0396   1.0000   0.0095
 -14.750  -1.3057   0.03355   0.02976  -0.0382   1.0000   0.0097
 -14.500  -1.3022   0.03193   0.02806  -0.0367   1.0000   0.0099
 -14.250  -1.2966   0.03055   0.02658  -0.0351   1.0000   0.0101
 -14.000  -1.2889   0.02938   0.02532  -0.0333   1.0000   0.0103
 -13.750  -1.2811   0.02824   0.02409  -0.0314   1.0000   0.0105
 -13.500  -1.2723   0.02721   0.02294  -0.0294   1.0000   0.0108
 -13.250  -1.2630   0.02622   0.02185  -0.0272   1.0000   0.0110
 -13.000  -1.2528   0.02530   0.02082  -0.0250   1.0000   0.0113
 -12.750  -1.2400   0.02447   0.01988  -0.0230   1.0000   0.0115
 -12.500  -1.2241   0.02374   0.01904  -0.0216   1.0000   0.0117
 -12.250  -1.2160   0.02220   0.01734  -0.0191   1.0000   0.0122
 -12.000  -1.2010   0.02131   0.01639  -0.0175   1.0000   0.0127
 -11.750  -1.1818   0.02081   0.01584  -0.0163   1.0000   0.0131
 -11.500  -1.1621   0.02036   0.01535  -0.0153   1.0000   0.0136
 -11.250  -1.1424   0.01990   0.01485  -0.0141   1.0000   0.0141
 -11.000  -1.1224   0.01950   0.01438  -0.0130   1.0000   0.0146
 -10.750  -1.1020   0.01917   0.01398  -0.0118   1.0000   0.0150
 -10.500  -1.0878   0.01823   0.01295  -0.0097   1.0000   0.0157
 -10.250  -1.0709   0.01766   0.01234  -0.0079   1.0000   0.0163
 -10.000  -1.0513   0.01739   0.01206  -0.0066   1.0000   0.0169
  -9.750  -1.0320   0.01711   0.01176  -0.0051   1.0000   0.0175
  -9.500  -1.0133   0.01681   0.01142  -0.0035   1.0000   0.0182
  -9.250  -0.9946   0.01652   0.01108  -0.0018   1.0000   0.0188
  -9.000  -0.9752   0.01635   0.01086  -0.0003   1.0000   0.0192
  -8.750  -0.9623   0.01543   0.00986   0.0023   1.0000   0.0202
  -8.500  -0.9444   0.01511   0.00954   0.0040   1.0000   0.0210
  -8.250  -0.9255   0.01488   0.00931   0.0056   1.0000   0.0218
  -8.000  -0.9067   0.01462   0.00902   0.0073   1.0000   0.0226
  -7.750  -0.8805   0.01432   0.00867   0.0073   0.9994   0.0235
  -7.500  -0.8486   0.01409   0.00841   0.0062   0.9983   0.0242
  -7.250  -0.8193   0.01335   0.00760   0.0054   0.9970   0.0254
  -7.000  -0.7889   0.01277   0.00701   0.0045   0.9958   0.0267
  -6.750  -0.7567   0.01241   0.00664   0.0032   0.9947   0.0278
  -6.500  -0.7245   0.01210   0.00631   0.0020   0.9937   0.0290
  -6.250  -0.6943   0.01181   0.00600   0.0013   0.9917   0.0300
  -6.000  -0.6630   0.01153   0.00569   0.0003   0.9898   0.0307
  -5.750  -0.6323   0.01103   0.00514  -0.0006   0.9880   0.0318
  -5.500  -0.6007   0.01053   0.00462  -0.0017   0.9865   0.0338
  -5.250  -0.5676   0.01021   0.00429  -0.0030   0.9853   0.0352
  -5.000  -0.5338   0.00992   0.00399  -0.0045   0.9843   0.0367
  -4.750  -0.4993   0.00968   0.00374  -0.0061   0.9835   0.0382
  -4.500  -0.4689   0.00943   0.00347  -0.0068   0.9809   0.0395
  -4.250  -0.4385   0.00910   0.00315  -0.0075   0.9780   0.0436
  -4.000  -0.4068   0.00885   0.00293  -0.0084   0.9755   0.0482
  -3.750  -0.3755   0.00848   0.00269  -0.0093   0.9732   0.0715
  -3.500  -0.3449   0.00809   0.00247  -0.0101   0.9708   0.1069
  -3.250  -0.3199   0.00774   0.00229  -0.0097   0.9656   0.1494
  -3.000  -0.2936   0.00737   0.00212  -0.0095   0.9607   0.2003
  -2.750  -0.2674   0.00693   0.00193  -0.0093   0.9565   0.2663
  -2.500  -0.2458   0.00639   0.00175  -0.0082   0.9497   0.3631
  -2.250  -0.2237   0.00581   0.00157  -0.0071   0.9436   0.4735
  -2.000  -0.2019   0.00531   0.00144  -0.0059   0.9370   0.5763
  -1.750  -0.1796   0.00493   0.00136  -0.0047   0.9299   0.6579
  -1.500  -0.1544   0.00474   0.00130  -0.0040   0.9236   0.7026
  -1.250  -0.1291   0.00460   0.00126  -0.0034   0.9161   0.7359
  -1.000  -0.1033   0.00448   0.00123  -0.0027   0.9092   0.7696
  -0.750  -0.0776   0.00439   0.00122  -0.0021   0.9000   0.7972
  -0.500  -0.0518   0.00433   0.00119  -0.0014   0.8881   0.8208
  -0.250  -0.0258   0.00428   0.00117  -0.0007   0.8733   0.8386
   0.000   0.0000   0.00427   0.00116   0.0000   0.8564   0.8562
   0.250   0.0258   0.00428   0.00117   0.0007   0.8387   0.8733
   0.500   0.0517   0.00433   0.00119   0.0014   0.8205   0.8882
   0.750   0.0776   0.00438   0.00122   0.0021   0.7977   0.9000
   1.000   0.1033   0.00448   0.00123   0.0027   0.7701   0.9092
   1.250   0.1291   0.00460   0.00126   0.0034   0.7357   0.9161
   1.500   0.1545   0.00474   0.00130   0.0040   0.7028   0.9236
   1.750   0.1796   0.00493   0.00136   0.0047   0.6583   0.9299
   2.000   0.2020   0.00530   0.00144   0.0059   0.5772   0.9369
   2.250   0.2237   0.00581   0.00157   0.0071   0.4738   0.9436
   2.500   0.2459   0.00638   0.00175   0.0082   0.3637   0.9496
   2.750   0.2674   0.00693   0.00193   0.0093   0.2661   0.9565
   3.000   0.2936   0.00737   0.00212   0.0095   0.2003   0.9607
   3.250   0.3199   0.00774   0.00229   0.0097   0.1493   0.9656
   3.500   0.3449   0.00809   0.00247   0.0101   0.1069   0.9708
   3.750   0.3755   0.00848   0.00269   0.0093   0.0714   0.9732
   4.000   0.4068   0.00885   0.00293   0.0084   0.0482   0.9755
   4.250   0.4385   0.00910   0.00315   0.0075   0.0437   0.9780
   4.500   0.4689   0.00943   0.00347   0.0068   0.0395   0.9809
   4.750   0.4992   0.00968   0.00374   0.0062   0.0382   0.9835
   5.000   0.5337   0.00992   0.00399   0.0045   0.0367   0.9843
   5.250   0.5676   0.01020   0.00428   0.0030   0.0352   0.9853
   5.500   0.6007   0.01053   0.00462   0.0017   0.0338   0.9865
   5.750   0.6323   0.01102   0.00513   0.0006   0.0319   0.9880
   6.000   0.6629   0.01153   0.00569  -0.0003   0.0307   0.9898
   6.250   0.6943   0.01181   0.00600  -0.0013   0.0300   0.9917
   6.500   0.7245   0.01209   0.00630  -0.0020   0.0289   0.9937
   6.750   0.7568   0.01241   0.00664  -0.0032   0.0278   0.9947
   7.000   0.7889   0.01277   0.00701  -0.0045   0.0267   0.9958
   7.250   0.8193   0.01335   0.00760  -0.0054   0.0254   0.9970
   7.500   0.8486   0.01409   0.00841  -0.0062   0.0242   0.9983
   7.750   0.8805   0.01432   0.00867  -0.0073   0.0235   0.9994
   8.000   0.9066   0.01462   0.00902  -0.0072   0.0226   1.0000
   8.250   0.9254   0.01488   0.00931  -0.0056   0.0218   1.0000
   8.500   0.9443   0.01511   0.00954  -0.0040   0.0210   1.0000
   8.750   0.9622   0.01543   0.00986  -0.0023   0.0202   1.0000
   9.000   0.9751   0.01635   0.01086   0.0003   0.0192   1.0000
   9.250   0.9946   0.01652   0.01108   0.0019   0.0188   1.0000
   9.500   1.0133   0.01681   0.01142   0.0035   0.0182   1.0000
   9.750   1.0320   0.01711   0.01176   0.0051   0.0175   1.0000
  10.000   1.0512   0.01739   0.01206   0.0066   0.0169   1.0000
  10.250   1.0708   0.01766   0.01235   0.0079   0.0163   1.0000
  10.500   1.0878   0.01823   0.01295   0.0097   0.0157   1.0000
  10.750   1.1021   0.01915   0.01397   0.0118   0.0150   1.0000
  11.000   1.1225   0.01948   0.01436   0.0130   0.0146   1.0000
  11.250   1.1425   0.01990   0.01484   0.0141   0.0141   1.0000
  11.500   1.1622   0.02036   0.01535   0.0152   0.0136   1.0000
  11.750   1.1820   0.02080   0.01584   0.0163   0.0131   1.0000
  12.000   1.2011   0.02131   0.01639   0.0174   0.0127   1.0000
  12.250   1.2163   0.02219   0.01734   0.0190   0.0122   1.0000
  12.500   1.2244   0.02374   0.01905   0.0215   0.0117   1.0000
  12.750   1.2404   0.02447   0.01988   0.0230   0.0115   1.0000
  13.000   1.2533   0.02530   0.02081   0.0249   0.0113   1.0000
  13.250   1.2635   0.02622   0.02185   0.0271   0.0110   1.0000
  13.500   1.2729   0.02720   0.02294   0.0292   0.0108   1.0000
  13.750   1.2819   0.02824   0.02408   0.0313   0.0105   1.0000
  14.000   1.2900   0.02935   0.02529   0.0332   0.0103   1.0000
  14.250   1.2972   0.03057   0.02660   0.0349   0.0101   1.0000
  14.500   1.3032   0.03192   0.02804   0.0365   0.0099   1.0000
  14.750   1.3066   0.03355   0.02977   0.0381   0.0097   1.0000
  15.000   1.3053   0.03570   0.03203   0.0394   0.0095   1.0000
  15.250   1.2969   0.03872   0.03520   0.0404   0.0093   1.0000
  15.500   1.2810   0.04288   0.03955   0.0406   0.0092   1.0000
  15.750   1.2599   0.04829   0.04519   0.0392   0.0091   1.0000
  16.000   1.2362   0.05503   0.05214   0.0359   0.0090   1.0000
  16.250   1.2140   0.06264   0.05994   0.0311   0.0090   1.0000
  16.500   1.1909   0.07157   0.06905   0.0249   0.0091   1.0000
  16.750   1.1649   0.08180   0.07945   0.0183   0.0092   1.0000
  17.000   1.1227   0.09525   0.09309   0.0106   0.0094   1.0000
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