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NACA 63 (naca633418-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 100,000
Max Cl/Cd: 44.68 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633418-il-100000-n5.txt
Download as CSV file: xf-naca633418-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63                                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7092   0.09247   0.08617  -0.0628   1.0000   0.0430
 -15.500  -0.7555   0.07844   0.07177  -0.0708   1.0000   0.0433
 -15.250  -0.7631   0.07424   0.06747  -0.0728   1.0000   0.0437
 -15.000  -0.7706   0.07027   0.06338  -0.0745   1.0000   0.0441
 -14.750  -0.7764   0.06670   0.05970  -0.0759   1.0000   0.0446
 -14.500  -0.7815   0.06340   0.05628  -0.0770   1.0000   0.0453
 -14.250  -0.7870   0.06012   0.05287  -0.0780   1.0000   0.0461
 -14.000  -0.7914   0.05700   0.04958  -0.0787   1.0000   0.0468
 -13.750  -0.7953   0.05407   0.04645  -0.0792   1.0000   0.0478
 -13.500  -0.7964   0.05138   0.04356  -0.0793   1.0000   0.0486
 -13.250  -0.7953   0.04898   0.04096  -0.0791   1.0000   0.0496
 -13.000  -0.7843   0.04746   0.03949  -0.0787   1.0000   0.0505
 -12.750  -0.7754   0.04589   0.03789  -0.0782   1.0000   0.0516
 -12.500  -0.7684   0.04429   0.03624  -0.0777   1.0000   0.0529
 -12.250  -0.7615   0.04272   0.03457  -0.0770   1.0000   0.0545
 -12.000  -0.7547   0.04120   0.03289  -0.0761   1.0000   0.0562
 -11.750  -0.7455   0.03997   0.03169  -0.0750   1.0000   0.0577
 -11.500  -0.7387   0.03887   0.03065  -0.0736   1.0000   0.0592
 -11.250  -0.7353   0.03787   0.02966  -0.0716   1.0000   0.0608
 -11.000  -0.7342   0.03698   0.02875  -0.0695   0.9979   0.0626
 -10.750  -0.7061   0.03557   0.02724  -0.0716   0.9825   0.0658
 -10.500  -0.6783   0.03420   0.02589  -0.0741   0.9705   0.0692
 -10.250  -0.6495   0.03296   0.02453  -0.0762   0.9590   0.0735
 -10.000  -0.6230   0.03163   0.02323  -0.0783   0.9476   0.0777
  -9.500  -0.5732   0.02920   0.02071  -0.0816   0.9245   0.0889
  -9.250  -0.5523   0.02817   0.01959  -0.0823   0.9125   0.0958
  -9.000  -0.5365   0.02702   0.01845  -0.0824   0.9008   0.1026
  -8.750  -0.5241   0.02611   0.01749  -0.0815   0.8883   0.1108
  -8.500  -0.5159   0.02524   0.01661  -0.0800   0.8764   0.1195
  -8.250  -0.5036   0.02435   0.01572  -0.0789   0.8670   0.1311
  -8.000  -0.4937   0.02357   0.01497  -0.0773   0.8560   0.1455
  -7.750  -0.4800   0.02272   0.01416  -0.0762   0.8479   0.1659
  -7.500  -0.4684   0.02189   0.01344  -0.0748   0.8382   0.1918
  -7.250  -0.4535   0.02099   0.01268  -0.0739   0.8312   0.2283
  -7.000  -0.4403   0.02024   0.01215  -0.0726   0.8220   0.2718
  -6.750  -0.4224   0.01960   0.01174  -0.0716   0.8153   0.3233
  -6.500  -0.4022   0.01930   0.01158  -0.0708   0.8079   0.3698
  -6.250  -0.3795   0.01917   0.01149  -0.0700   0.8008   0.4060
  -6.000  -0.3541   0.01908   0.01133  -0.0696   0.7954   0.4345
  -5.750  -0.3304   0.01911   0.01132  -0.0690   0.7878   0.4565
  -5.500  -0.3047   0.01916   0.01130  -0.0685   0.7815   0.4754
  -5.250  -0.2776   0.01920   0.01123  -0.0682   0.7766   0.4926
  -5.000  -0.2533   0.01930   0.01126  -0.0677   0.7690   0.5081
  -4.750  -0.2269   0.01942   0.01130  -0.0672   0.7631   0.5219
  -4.500  -0.1991   0.01958   0.01139  -0.0666   0.7586   0.5335
  -4.250  -0.1743   0.01967   0.01142  -0.0662   0.7512   0.5451
  -4.000  -0.1477   0.01978   0.01146  -0.0657   0.7454   0.5546
  -3.750  -0.1199   0.01975   0.01131  -0.0655   0.7409   0.5633
  -3.500  -0.0945   0.01985   0.01139  -0.0650   0.7343   0.5704
  -3.250  -0.0679   0.01975   0.01116  -0.0651   0.7283   0.5790
  -3.000  -0.0401   0.01978   0.01114  -0.0647   0.7238   0.5841
  -2.750  -0.0138   0.01978   0.01108  -0.0646   0.7180   0.5909
  -2.500   0.0126   0.01972   0.01093  -0.0646   0.7119   0.5977
  -2.250   0.0401   0.01972   0.01090  -0.0643   0.7071   0.6024
  -2.000   0.0678   0.01968   0.01078  -0.0643   0.7025   0.6085
  -1.750   0.0938   0.01965   0.01069  -0.0644   0.6962   0.6152
  -1.500   0.1206   0.01968   0.01071  -0.0641   0.6912   0.6194
  -1.250   0.1492   0.01964   0.01059  -0.0641   0.6872   0.6248
  -1.000   0.1755   0.01963   0.01053  -0.0643   0.6811   0.6316
  -0.750   0.2016   0.01968   0.01060  -0.0640   0.6756   0.6359
  -0.500   0.2293   0.01969   0.01058  -0.0639   0.6714   0.6407
  -0.250   0.2579   0.01967   0.01049  -0.0641   0.6674   0.6468
   0.000   0.2830   0.01976   0.01059  -0.0641   0.6610   0.6524
   0.250   0.3094   0.01981   0.01067  -0.0637   0.6561   0.6568
   0.500   0.3381   0.01981   0.01062  -0.0639   0.6523   0.6624
   0.750   0.3654   0.01988   0.01067  -0.0642   0.6473   0.6692
   1.000   0.3897   0.02002   0.01088  -0.0637   0.6417   0.6732
   1.250   0.4169   0.02007   0.01094  -0.0635   0.6372   0.6784
   1.500   0.4469   0.02005   0.01087  -0.0639   0.6337   0.6849
   1.750   0.4705   0.02028   0.01117  -0.0636   0.6279   0.6904
   2.000   0.4954   0.02042   0.01137  -0.0631   0.6226   0.6952
   2.250   0.5238   0.02045   0.01141  -0.0633   0.6185   0.7013
   2.500   0.5529   0.02050   0.01143  -0.0636   0.6147   0.7078
   2.750   0.5739   0.02080   0.01188  -0.0627   0.6084   0.7128
   3.000   0.6002   0.02092   0.01204  -0.0625   0.6035   0.7190
   3.250   0.6302   0.02093   0.01203  -0.0630   0.5997   0.7256
   3.500   0.6526   0.02118   0.01239  -0.0621   0.5943   0.7309
   3.750   0.6759   0.02141   0.01271  -0.0616   0.5884   0.7376
   4.000   0.7041   0.02147   0.01279  -0.0618   0.5839   0.7443
   4.250   0.7312   0.02152   0.01290  -0.0615   0.5797   0.7499
   4.500   0.7509   0.02191   0.01342  -0.0606   0.5726   0.7572
   4.750   0.7770   0.02200   0.01358  -0.0603   0.5675   0.7639
   5.000   0.8067   0.02196   0.01356  -0.0603   0.5635   0.7704
   5.250   0.8247   0.02242   0.01418  -0.0593   0.5557   0.7787
   5.500   0.8487   0.02250   0.01435  -0.0585   0.5501   0.7849
   5.750   0.8777   0.02248   0.01437  -0.0586   0.5451   0.7927
   6.000   0.8936   0.02289   0.01495  -0.0570   0.5368   0.8004
   6.250   0.9213   0.02280   0.01492  -0.0567   0.5307   0.8082
   6.500   0.9391   0.02309   0.01534  -0.0553   0.5222   0.8168
   6.750   0.9633   0.02303   0.01535  -0.0544   0.5144   0.8253
   7.000   0.9808   0.02326   0.01571  -0.0529   0.5054   0.8346
   7.250   1.0039   0.02319   0.01571  -0.0519   0.4967   0.8443
   7.500   1.0167   0.02345   0.01613  -0.0496   0.4862   0.8549
   7.750   1.0374   0.02338   0.01610  -0.0482   0.4755   0.8666
   8.000   1.0495   0.02349   0.01633  -0.0457   0.4629   0.8799
   8.250   1.0565   0.02374   0.01670  -0.0425   0.4495   0.8965
   8.500   1.0634   0.02394   0.01699  -0.0393   0.4357   0.9183
   8.750   1.0759   0.02423   0.01737  -0.0375   0.4195   0.9546
   9.000   1.0885   0.02481   0.01798  -0.0365   0.4017   1.0000
   9.250   1.0996   0.02563   0.01879  -0.0354   0.3827   1.0000
   9.500   1.1093   0.02656   0.01966  -0.0342   0.3619   1.0000
   9.750   1.1155   0.02780   0.02085  -0.0328   0.3389   1.0000
  10.000   1.1201   0.02918   0.02211  -0.0314   0.3144   1.0000
  10.250   1.1223   0.03085   0.02367  -0.0300   0.2894   1.0000
  10.500   1.1219   0.03279   0.02547  -0.0286   0.2652   1.0000
  10.750   1.1208   0.03495   0.02751  -0.0274   0.2414   1.0000
  11.000   1.1181   0.03733   0.02977  -0.0263   0.2190   1.0000
  11.250   1.1153   0.03985   0.03219  -0.0254   0.1985   1.0000
  11.500   1.1132   0.04244   0.03469  -0.0247   0.1796   1.0000
  11.750   1.1111   0.04511   0.03729  -0.0242   0.1627   1.0000
  12.000   1.1096   0.04783   0.03995  -0.0238   0.1476   1.0000
  12.250   1.1089   0.05057   0.04265  -0.0236   0.1345   1.0000
  12.500   1.1086   0.05337   0.04541  -0.0234   0.1231   1.0000
  12.750   1.1084   0.05624   0.04823  -0.0234   0.1134   1.0000
  13.000   1.1110   0.05890   0.05091  -0.0235   0.1045   1.0000
  13.250   1.1129   0.06168   0.05368  -0.0236   0.0976   1.0000
  13.500   1.1154   0.06445   0.05648  -0.0239   0.0913   1.0000
  13.750   1.1184   0.06720   0.05923  -0.0241   0.0861   1.0000
  14.000   1.1225   0.06989   0.06198  -0.0244   0.0811   1.0000
  14.250   1.1249   0.07279   0.06484  -0.0248   0.0773   1.0000
  14.500   1.1312   0.07528   0.06743  -0.0251   0.0731   1.0000
  14.750   1.1352   0.07806   0.07025  -0.0256   0.0699   1.0000
  15.000   1.1402   0.08072   0.07292  -0.0260   0.0670   1.0000
  15.250   1.1464   0.08333   0.07564  -0.0265   0.0638   1.0000
  15.500   1.1514   0.08608   0.07843  -0.0271   0.0613   1.0000
  15.750   1.1573   0.08862   0.08092  -0.0276   0.0592   1.0000
  16.000   1.1640   0.09126   0.08373  -0.0281   0.0569   1.0000
  16.250   1.1697   0.09402   0.08659  -0.0288   0.0548   1.0000
  16.500   1.1750   0.09682   0.08943  -0.0296   0.0530   1.0000
  16.750   1.1823   0.09923   0.09181  -0.0302   0.0514   1.0000
  17.000   1.1863   0.10238   0.09517  -0.0311   0.0499   1.0000
  17.250   1.1899   0.10561   0.09855  -0.0322   0.0484   1.0000
  17.500   1.1933   0.10883   0.10187  -0.0334   0.0470   1.0000
  17.750   1.1982   0.11175   0.10482  -0.0345   0.0458   1.0000
  18.000   1.2056   0.11420   0.10726  -0.0354   0.0446   1.0000
  18.250   1.2021   0.11880   0.11213  -0.0375   0.0436   1.0000
  18.500   1.1988   0.12339   0.11692  -0.0397   0.0427   1.0000
  18.750   1.1953   0.12808   0.12180  -0.0421   0.0418   1.0000
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