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NACA 63-210 AIRFOIL (n63210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-210 AIRFOIL (n63210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 66.35 at α=11°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63210-il-1000000-n5.txt
Download as CSV file: xf-n63210-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-210 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -1.0246   0.05371   0.05159  -0.0403   1.0000   0.0030
 -14.000  -1.0590   0.04551   0.04315  -0.0456   1.0000   0.0029
 -13.750  -1.0802   0.04019   0.03763  -0.0479   1.0000   0.0029
 -13.500  -1.0886   0.03696   0.03425  -0.0485   1.0000   0.0030
 -13.250  -1.1008   0.03385   0.03094  -0.0480   1.0000   0.0029
 -13.000  -1.1081   0.03162   0.02856  -0.0462   1.0000   0.0030
 -12.750  -1.1096   0.02970   0.02647  -0.0443   1.0000   0.0031
 -12.500  -1.1023   0.02792   0.02452  -0.0431   1.0000   0.0031
 -12.250  -1.0918   0.02627   0.02270  -0.0421   1.0000   0.0032
 -12.000  -1.0785   0.02478   0.02105  -0.0412   1.0000   0.0033
 -11.750  -1.0632   0.02339   0.01949  -0.0405   1.0000   0.0034
 -11.500  -1.0459   0.02218   0.01812  -0.0398   1.0000   0.0035
 -11.250  -1.0272   0.02104   0.01685  -0.0392   1.0000   0.0036
 -11.000  -1.0074   0.02004   0.01571  -0.0387   1.0000   0.0037
 -10.750  -0.9865   0.01914   0.01468  -0.0382   1.0000   0.0037
 -10.500  -0.9652   0.01827   0.01368  -0.0378   1.0000   0.0038
 -10.250  -0.9430   0.01751   0.01282  -0.0373   1.0000   0.0039
 -10.000  -0.9212   0.01663   0.01183  -0.0369   1.0000   0.0041
  -9.750  -0.8986   0.01590   0.01100  -0.0364   1.0000   0.0044
  -9.500  -0.8757   0.01523   0.01025  -0.0360   1.0000   0.0046
  -9.250  -0.8529   0.01458   0.00954  -0.0355   1.0000   0.0050
  -9.000  -0.8231   0.01394   0.00881  -0.0365   0.9932   0.0053
  -8.750  -0.7920   0.01336   0.00816  -0.0377   0.9866   0.0058
  -8.500  -0.7604   0.01300   0.00779  -0.0388   0.9801   0.0066
  -8.000  -0.6970   0.01318   0.00809  -0.0407   0.9649   0.0104
  -7.750  -0.6683   0.01326   0.00815  -0.0409   0.9548   0.0118
  -7.500  -0.6403   0.01351   0.00838  -0.0409   0.9424   0.0123
  -7.250  -0.6139   0.01368   0.00850  -0.0405   0.9214   0.0125
  -7.000  -0.5931   0.01287   0.00751  -0.0394   0.8866   0.0131
  -6.750  -0.5694   0.01237   0.00688  -0.0389   0.8693   0.0136
  -6.500  -0.5437   0.01206   0.00651  -0.0387   0.8584   0.0141
  -6.250  -0.5172   0.01187   0.00625  -0.0386   0.8500   0.0147
  -6.000  -0.4902   0.01169   0.00605  -0.0386   0.8419   0.0155
  -5.750  -0.4635   0.01140   0.00570  -0.0386   0.8346   0.0160
  -5.500  -0.4368   0.01103   0.00526  -0.0385   0.8265   0.0161
  -5.250  -0.4099   0.01069   0.00487  -0.0385   0.8187   0.0164
  -5.000  -0.3828   0.01044   0.00456  -0.0385   0.8101   0.0168
  -4.750  -0.3555   0.01012   0.00419  -0.0385   0.8014   0.0170
  -4.500  -0.3284   0.00979   0.00379  -0.0385   0.7926   0.0169
  -4.250  -0.3010   0.00948   0.00342  -0.0385   0.7831   0.0169
  -4.000  -0.2734   0.00921   0.00308  -0.0386   0.7743   0.0168
  -3.750  -0.2458   0.00898   0.00277  -0.0386   0.7653   0.0167
  -3.500  -0.2179   0.00876   0.00251  -0.0387   0.7565   0.0167
  -3.250  -0.1899   0.00858   0.00226  -0.0388   0.7482   0.0166
  -3.000  -0.1618   0.00841   0.00204  -0.0388   0.7396   0.0166
  -2.750  -0.1337   0.00826   0.00185  -0.0390   0.7315   0.0166
  -2.500  -0.1055   0.00814   0.00168  -0.0391   0.7231   0.0166
  -2.250  -0.0771   0.00802   0.00153  -0.0392   0.7147   0.0166
  -2.000  -0.0489   0.00793   0.00140  -0.0393   0.7065   0.0166
  -1.750  -0.0204   0.00784   0.00129  -0.0394   0.6980   0.0167
  -1.500   0.0080   0.00777   0.00119  -0.0395   0.6900   0.0168
  -1.250   0.0364   0.00771   0.00110  -0.0397   0.6813   0.0170
  -1.000   0.0648   0.00765   0.00103  -0.0398   0.6732   0.0175
  -0.750   0.0932   0.00761   0.00097  -0.0399   0.6647   0.0181
  -0.500   0.1216   0.00758   0.00093  -0.0401   0.6527   0.0229
  -0.250   0.1482   0.00622   0.00067  -0.0410   0.6240   0.4133
   0.000   0.1758   0.00593   0.00066  -0.0412   0.6004   0.5178
   0.250   0.2038   0.00593   0.00071  -0.0414   0.5781   0.5651
   0.500   0.2319   0.00604   0.00074  -0.0414   0.5516   0.5785
   0.750   0.2596   0.00620   0.00077  -0.0415   0.5132   0.5876
   1.000   0.2863   0.00651   0.00084  -0.0414   0.4443   0.5987
   1.250   0.3108   0.00721   0.00105  -0.0413   0.3031   0.6159
   1.500   0.3317   0.00867   0.00155  -0.0408   0.0207   0.6344
   1.750   0.3598   0.00874   0.00165  -0.0409   0.0192   0.6457
   2.000   0.3878   0.00883   0.00177  -0.0410   0.0183   0.6568
   2.250   0.4158   0.00893   0.00190  -0.0411   0.0176   0.6710
   2.500   0.4437   0.00903   0.00203  -0.0411   0.0171   0.6855
   2.750   0.4715   0.00915   0.00219  -0.0412   0.0167   0.6986
   3.000   0.4993   0.00928   0.00237  -0.0412   0.0163   0.7107
   3.250   0.5269   0.00943   0.00255  -0.0412   0.0159   0.7221
   3.500   0.5544   0.00960   0.00277  -0.0412   0.0154   0.7333
   3.750   0.5817   0.00980   0.00304  -0.0411   0.0149   0.7441
   4.000   0.6086   0.01006   0.00337  -0.0410   0.0143   0.7546
   4.250   0.6349   0.01042   0.00381  -0.0408   0.0138   0.7658
   4.500   0.6617   0.01068   0.00412  -0.0407   0.0137   0.7776
   4.750   0.6881   0.01096   0.00448  -0.0405   0.0137   0.7886
   5.000   0.7143   0.01128   0.00486  -0.0403   0.0136   0.7989
   5.250   0.7402   0.01163   0.00527  -0.0400   0.0135   0.8094
   5.750   0.7907   0.01246   0.00625  -0.0393   0.0135   0.8323
   6.000   0.8152   0.01292   0.00681  -0.0389   0.0134   0.8448
   6.250   0.8391   0.01343   0.00742  -0.0383   0.0134   0.8589
   6.500   0.8622   0.01398   0.00807  -0.0375   0.0134   0.8756
   6.750   0.8859   0.01437   0.00855  -0.0369   0.0133   0.8913
   7.000   0.9104   0.01451   0.00874  -0.0364   0.0129   0.9075
   7.250   0.9338   0.01474   0.00905  -0.0356   0.0125   0.9242
   7.500   0.9551   0.01517   0.00956  -0.0345   0.0123   0.9434
   8.000   1.0044   0.01596   0.01047  -0.0339   0.0116   1.0000
   8.250   1.0300   0.01623   0.01075  -0.0338   0.0110   1.0000
   8.500   1.0543   0.01668   0.01124  -0.0335   0.0108   1.0000
   8.750   1.0789   0.01703   0.01163  -0.0332   0.0104   1.0000
   9.000   1.1039   0.01729   0.01189  -0.0331   0.0101   1.0000
   9.250   1.1286   0.01757   0.01218  -0.0329   0.0097   1.0000
   9.500   1.1512   0.01812   0.01275  -0.0324   0.0093   1.0000
   9.750   1.1751   0.01847   0.01313  -0.0321   0.0091   1.0000
  10.000   1.2005   0.01863   0.01332  -0.0319   0.0088   1.0000
  10.250   1.2240   0.01903   0.01380  -0.0315   0.0081   1.0000
  10.500   1.2385   0.02067   0.01571  -0.0299   0.0059   1.0000
  10.750   1.2717   0.01959   0.01442  -0.0309   0.0055   1.0000
  11.000   1.2978   0.01956   0.01426  -0.0309   0.0049   1.0000
  11.250   1.3192   0.02007   0.01477  -0.0303   0.0043   1.0000
  11.500   1.3377   0.02085   0.01563  -0.0293   0.0040   1.0000
  11.750   1.3549   0.02171   0.01659  -0.0281   0.0038   1.0000
  12.000   1.3705   0.02264   0.01763  -0.0268   0.0036   1.0000
  12.250   1.3850   0.02360   0.01871  -0.0254   0.0035   1.0000
  12.500   1.3955   0.02461   0.01982  -0.0233   0.0033   1.0000
  12.750   1.4027   0.02573   0.02106  -0.0209   0.0032   1.0000
  13.000   1.4097   0.02689   0.02233  -0.0187   0.0031   1.0000
  13.250   1.4151   0.02824   0.02380  -0.0166   0.0030   1.0000
  13.500   1.4203   0.02967   0.02534  -0.0148   0.0029   1.0000
  13.750   1.4223   0.03147   0.02728  -0.0131   0.0027   1.0000
  14.000   1.4244   0.03337   0.02931  -0.0117   0.0026   1.0000
  14.250   1.4249   0.03552   0.03159  -0.0106   0.0025   1.0000
  14.500   1.4242   0.03788   0.03409  -0.0098   0.0025   1.0000
  14.750   1.4217   0.04060   0.03696  -0.0093   0.0024   1.0000
  15.000   1.4184   0.04356   0.04006  -0.0091   0.0024   1.0000
  15.250   1.4134   0.04689   0.04356  -0.0094   0.0024   1.0000
  15.500   1.4068   0.05062   0.04743  -0.0101   0.0024   1.0000
  15.750   1.3992   0.05472   0.05168  -0.0114   0.0024   1.0000
  16.000   1.3875   0.05967   0.05678  -0.0133   0.0024   1.0000
  16.250   1.3725   0.06547   0.06275  -0.0159   0.0024   1.0000
  16.500   1.3528   0.07254   0.06999  -0.0196   0.0024   1.0000
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