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NACA 63 (naca633418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.93 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633418-il-1000000-n5.txt
Download as CSV file: xf-naca633418-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0901   0.08701   0.08322  -0.0531   1.0000   0.0142
 -19.500  -1.0992   0.08229   0.07840  -0.0553   1.0000   0.0142
 -19.250  -1.1022   0.07855   0.07458  -0.0570   1.0000   0.0145
 -19.000  -1.1099   0.07419   0.07013  -0.0590   1.0000   0.0145
 -18.750  -1.1139   0.07038   0.06625  -0.0606   1.0000   0.0146
 -18.500  -1.1198   0.06645   0.06223  -0.0623   1.0000   0.0147
 -18.250  -1.1237   0.06280   0.05853  -0.0638   1.0000   0.0150
 -18.000  -1.1260   0.05945   0.05511  -0.0651   1.0000   0.0152
 -17.750  -1.1261   0.05643   0.05201  -0.0662   1.0000   0.0152
 -17.500  -1.1258   0.05353   0.04905  -0.0672   1.0000   0.0153
 -17.250  -1.1211   0.05116   0.04665  -0.0680   1.0000   0.0159
 -17.000  -1.1182   0.04863   0.04407  -0.0687   1.0000   0.0161
 -16.750  -1.1166   0.04604   0.04140  -0.0694   1.0000   0.0161
 -16.500  -1.1091   0.04412   0.03944  -0.0699   1.0000   0.0165
 -16.250  -1.1047   0.04191   0.03717  -0.0704   1.0000   0.0166
 -16.000  -1.0992   0.03988   0.03508  -0.0708   1.0000   0.0168
 -15.750  -1.0919   0.03809   0.03324  -0.0710   1.0000   0.0171
 -15.500  -1.0856   0.03628   0.03137  -0.0711   1.0000   0.0172
 -15.250  -1.0783   0.03460   0.02963  -0.0711   1.0000   0.0173
 -15.000  -1.0726   0.03282   0.02781  -0.0711   1.0000   0.0176
 -14.750  -1.0658   0.03118   0.02614  -0.0710   1.0000   0.0180
 -14.500  -1.0603   0.02965   0.02459  -0.0701   0.9782   0.0183
 -14.250  -1.0122   0.02794   0.02282  -0.0777   0.9561   0.0190
 -14.000  -0.9596   0.02638   0.02116  -0.0859   0.9314   0.0197
 -13.750  -0.9352   0.02530   0.01988  -0.0880   0.8906   0.0201
 -13.500  -0.9256   0.02433   0.01877  -0.0870   0.8667   0.0204
 -13.000  -0.9074   0.02232   0.01658  -0.0850   0.8366   0.0213
 -12.750  -0.8971   0.02139   0.01558  -0.0839   0.8250   0.0217
 -12.500  -0.8862   0.02054   0.01466  -0.0828   0.8142   0.0222
 -12.250  -0.8741   0.01972   0.01379  -0.0818   0.8049   0.0228
 -12.000  -0.8619   0.01898   0.01297  -0.0807   0.7957   0.0234
 -11.750  -0.8486   0.01827   0.01221  -0.0797   0.7877   0.0239
 -11.500  -0.8369   0.01755   0.01143  -0.0783   0.7792   0.0245
 -11.250  -0.8254   0.01686   0.01069  -0.0769   0.7715   0.0252
 -11.000  -0.8146   0.01622   0.01001  -0.0752   0.7638   0.0260
 -10.750  -0.8063   0.01570   0.00943  -0.0729   0.7569   0.0267
 -10.500  -0.7910   0.01526   0.00895  -0.0716   0.7505   0.0276
 -10.250  -0.7727   0.01485   0.00850  -0.0706   0.7437   0.0286
 -10.000  -0.7532   0.01445   0.00807  -0.0698   0.7374   0.0299
  -9.750  -0.7317   0.01410   0.00769  -0.0692   0.7311   0.0313
  -9.500  -0.7092   0.01380   0.00733  -0.0687   0.7251   0.0324
  -9.250  -0.6868   0.01344   0.00696  -0.0682   0.7197   0.0341
  -9.000  -0.6630   0.01313   0.00663  -0.0679   0.7137   0.0360
  -8.750  -0.6386   0.01287   0.00632  -0.0677   0.7074   0.0376
  -8.500  -0.6144   0.01256   0.00601  -0.0674   0.7018   0.0401
  -8.250  -0.5890   0.01229   0.00573  -0.0673   0.6963   0.0427
  -8.000  -0.5637   0.01202   0.00543  -0.0672   0.6902   0.0457
  -7.750  -0.5379   0.01178   0.00517  -0.0671   0.6846   0.0489
  -7.500  -0.5118   0.01151   0.00491  -0.0671   0.6792   0.0532
  -7.250  -0.4853   0.01127   0.00466  -0.0671   0.6734   0.0580
  -7.000  -0.4589   0.01103   0.00442  -0.0671   0.6680   0.0639
  -6.750  -0.4320   0.01077   0.00419  -0.0672   0.6626   0.0712
  -6.500  -0.4050   0.01053   0.00396  -0.0673   0.6568   0.0793
  -6.000  -0.3506   0.01003   0.00352  -0.0676   0.6465   0.1026
  -5.750  -0.3232   0.00977   0.00331  -0.0678   0.6409   0.1183
  -5.500  -0.2957   0.00952   0.00310  -0.0680   0.6354   0.1377
  -5.250  -0.2682   0.00922   0.00289  -0.0683   0.6310   0.1614
  -5.000  -0.2404   0.00889   0.00268  -0.0686   0.6263   0.1910
  -4.750  -0.2126   0.00857   0.00247  -0.0689   0.6210   0.2255
  -4.250  -0.1566   0.00790   0.00208  -0.0697   0.6114   0.3066
  -4.000  -0.1280   0.00763   0.00194  -0.0701   0.6067   0.3446
  -3.750  -0.0992   0.00743   0.00183  -0.0705   0.6020   0.3787
  -3.500  -0.0701   0.00733   0.00176  -0.0708   0.5977   0.4021
  -3.250  -0.0406   0.00724   0.00171  -0.0712   0.5935   0.4193
  -3.000  -0.0111   0.00717   0.00166  -0.0716   0.5887   0.4352
  -2.750   0.0182   0.00712   0.00163  -0.0719   0.5836   0.4488
  -2.500   0.0476   0.00709   0.00160  -0.0723   0.5795   0.4603
  -2.250   0.0773   0.00707   0.00158  -0.0727   0.5756   0.4708
  -2.000   0.1069   0.00703   0.00157  -0.0730   0.5713   0.4801
  -1.750   0.1364   0.00704   0.00156  -0.0734   0.5669   0.4871
  -1.500   0.1658   0.00705   0.00155  -0.0737   0.5625   0.4935
  -1.250   0.1955   0.00704   0.00155  -0.0741   0.5583   0.5000
  -1.000   0.2252   0.00705   0.00155  -0.0744   0.5540   0.5052
  -0.750   0.2546   0.00706   0.00155  -0.0747   0.5498   0.5103
  -0.500   0.2839   0.00708   0.00156  -0.0751   0.5456   0.5156
  -0.250   0.3136   0.00709   0.00158  -0.0754   0.5418   0.5206
   0.000   0.3431   0.00712   0.00159  -0.0758   0.5373   0.5248
   0.250   0.3724   0.00714   0.00162  -0.0761   0.5330   0.5294
   0.500   0.4016   0.00718   0.00165  -0.0764   0.5287   0.5343
   0.750   0.4312   0.00720   0.00168  -0.0767   0.5250   0.5390
   1.000   0.4606   0.00724   0.00171  -0.0770   0.5203   0.5427
   1.250   0.4897   0.00727   0.00175  -0.0773   0.5156   0.5474
   1.500   0.5187   0.00733   0.00180  -0.0776   0.5109   0.5524
   1.750   0.5481   0.00736   0.00185  -0.0779   0.5064   0.5570
   2.000   0.5772   0.00741   0.00190  -0.0782   0.5012   0.5608
   2.250   0.6059   0.00748   0.00196  -0.0784   0.4961   0.5654
   2.500   0.6350   0.00752   0.00203  -0.0787   0.4916   0.5706
   2.750   0.6640   0.00757   0.00209  -0.0790   0.4863   0.5754
   3.000   0.6925   0.00765   0.00217  -0.0791   0.4805   0.5796
   3.250   0.7212   0.00772   0.00225  -0.0794   0.4755   0.5843
   3.500   0.7499   0.00778   0.00233  -0.0796   0.4690   0.5891
   3.750   0.7778   0.00791   0.00243  -0.0797   0.4605   0.5940
   4.000   0.8061   0.00799   0.00253  -0.0799   0.4516   0.5988
   4.250   0.8338   0.00811   0.00264  -0.0799   0.4435   0.6041
   4.500   0.8620   0.00820   0.00275  -0.0801   0.4355   0.6091
   4.750   0.8891   0.00836   0.00288  -0.0800   0.4247   0.6135
   5.000   0.9153   0.00856   0.00304  -0.0799   0.4066   0.6182
   5.250   0.9402   0.00884   0.00324  -0.0795   0.3818   0.6238
   5.500   0.9649   0.00915   0.00346  -0.0791   0.3598   0.6292
   5.750   0.9891   0.00946   0.00369  -0.0787   0.3369   0.6339
   6.000   1.0118   0.00986   0.00399  -0.0780   0.3117   0.6389
   6.250   1.0329   0.01034   0.00434  -0.0771   0.2818   0.6441
   6.500   1.0517   0.01094   0.00477  -0.0758   0.2472   0.6492
   6.750   1.0696   0.01153   0.00521  -0.0745   0.2150   0.6542
   7.000   1.0880   0.01206   0.00563  -0.0731   0.1890   0.6600
   7.250   1.1049   0.01261   0.00608  -0.0716   0.1652   0.6654
   7.500   1.1218   0.01313   0.00651  -0.0700   0.1462   0.6701
   7.750   1.1369   0.01363   0.00695  -0.0681   0.1297   0.6755
   8.000   1.1472   0.01413   0.00740  -0.0653   0.1147   0.6818
   8.250   1.1573   0.01471   0.00792  -0.0626   0.1014   0.6872
   8.500   1.1682   0.01528   0.00848  -0.0602   0.0906   0.6930
   8.750   1.1792   0.01590   0.00907  -0.0579   0.0811   0.6990
   9.000   1.1903   0.01656   0.00972  -0.0558   0.0732   0.7050
   9.250   1.2003   0.01730   0.01046  -0.0537   0.0656   0.7111
   9.750   1.2233   0.01882   0.01200  -0.0503   0.0556   0.7242
  10.000   1.2339   0.01968   0.01288  -0.0486   0.0514   0.7308
  10.250   1.2461   0.02051   0.01374  -0.0472   0.0481   0.7383
  10.500   1.2562   0.02149   0.01474  -0.0457   0.0446   0.7453
  10.750   1.2684   0.02239   0.01568  -0.0444   0.0422   0.7531
  11.000   1.2788   0.02344   0.01676  -0.0431   0.0397   0.7607
  11.250   1.2897   0.02447   0.01784  -0.0419   0.0378   0.7695
  11.500   1.3005   0.02556   0.01898  -0.0408   0.0357   0.7786
  11.750   1.3100   0.02676   0.02022  -0.0397   0.0338   0.7881
  12.000   1.3201   0.02795   0.02147  -0.0386   0.0321   0.7980
  12.250   1.3295   0.02920   0.02279  -0.0376   0.0306   0.8105
  12.500   1.3377   0.03058   0.02422  -0.0366   0.0291   0.8237
  12.750   1.3466   0.03190   0.02564  -0.0357   0.0281   0.8402
  13.000   1.3545   0.03328   0.02712  -0.0346   0.0270   0.8620
  13.250   1.3600   0.03466   0.02864  -0.0332   0.0259   0.9040
  14.250   1.3949   0.04145   0.03567  -0.0321   0.0223   1.0000
  14.500   1.4022   0.04335   0.03761  -0.0318   0.0217   1.0000
  14.750   1.4079   0.04543   0.03973  -0.0315   0.0210   1.0000
  15.000   1.4158   0.04736   0.04170  -0.0314   0.0206   1.0000
  15.250   1.4228   0.04940   0.04380  -0.0313   0.0201   1.0000
  15.500   1.4288   0.05161   0.04605  -0.0313   0.0196   1.0000
  15.750   1.4350   0.05381   0.04830  -0.0313   0.0191   1.0000
  16.000   1.4395   0.05626   0.05079  -0.0315   0.0186   1.0000
  16.250   1.4438   0.05877   0.05334  -0.0317   0.0180   1.0000
  16.500   1.4479   0.06136   0.05598  -0.0320   0.0177   1.0000
  16.750   1.4532   0.06386   0.05855  -0.0323   0.0173   1.0000
  17.000   1.4578   0.06645   0.06121  -0.0327   0.0170   1.0000
  17.250   1.4615   0.06924   0.06405  -0.0333   0.0166   1.0000
  17.500   1.4654   0.07201   0.06688  -0.0338   0.0162   1.0000
  17.750   1.4674   0.07509   0.07003  -0.0345   0.0160   1.0000
  18.000   1.4698   0.07815   0.07314  -0.0353   0.0156   1.0000
  18.250   1.4705   0.08149   0.07653  -0.0362   0.0153   1.0000
  18.500   1.4706   0.08498   0.08009  -0.0372   0.0150   1.0000
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