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NACA 63(2)A-015 (naca632a015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)A-015 (naca632a015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 84.88 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca632a015-il-1000000-n5.txt
Download as CSV file: xf-naca632a015-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)A-015                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9410   0.08902   0.08654  -0.0380   1.0000   0.0058
 -17.250  -0.9750   0.07862   0.07594  -0.0441   1.0000   0.0060
 -17.000  -1.0117   0.06902   0.06612  -0.0494   1.0000   0.0058
 -16.750  -1.0320   0.06270   0.05964  -0.0524   1.0000   0.0059
 -16.500  -1.0437   0.05796   0.05474  -0.0542   1.0000   0.0060
 -16.250  -1.0587   0.05313   0.04975  -0.0558   1.0000   0.0060
 -16.000  -1.0644   0.04967   0.04616  -0.0566   1.0000   0.0060
 -15.750  -1.0732   0.04606   0.04241  -0.0571   1.0000   0.0060
 -15.500  -1.0780   0.04301   0.03922  -0.0571   1.0000   0.0060
 -15.250  -1.0798   0.04040   0.03649  -0.0570   1.0000   0.0060
 -15.000  -1.0796   0.03808   0.03405  -0.0565   1.0000   0.0061
 -14.750  -1.0786   0.03591   0.03177  -0.0559   1.0000   0.0060
 -14.500  -1.0705   0.03444   0.03021  -0.0552   1.0000   0.0062
 -14.250  -1.0680   0.03251   0.02816  -0.0542   1.0000   0.0062
 -14.000  -1.0620   0.03096   0.02650  -0.0532   1.0000   0.0062
 -13.750  -1.0574   0.02936   0.02481  -0.0519   1.0000   0.0062
 -13.500  -1.0481   0.02816   0.02351  -0.0507   1.0000   0.0063
 -13.250  -1.0375   0.02711   0.02238  -0.0494   1.0000   0.0063
 -13.000  -1.0288   0.02597   0.02116  -0.0478   1.0000   0.0063
 -12.750  -1.0225   0.02468   0.01978  -0.0459   1.0000   0.0064
 -12.500  -1.0145   0.02358   0.01860  -0.0439   1.0000   0.0065
 -12.250  -1.0055   0.02262   0.01756  -0.0419   1.0000   0.0066
 -12.000  -0.9951   0.02182   0.01671  -0.0398   1.0000   0.0067
 -11.750  -0.9834   0.02118   0.01604  -0.0378   1.0000   0.0069
 -11.500  -0.9731   0.02051   0.01532  -0.0353   1.0000   0.0070
 -11.250  -0.9651   0.01980   0.01455  -0.0324   1.0000   0.0069
 -11.000  -0.9559   0.01931   0.01403  -0.0295   1.0000   0.0070
 -10.750  -0.9322   0.01861   0.01328  -0.0295   0.9934   0.0072
 -10.250  -0.8743   0.01725   0.01182  -0.0315   0.9711   0.0074
 -10.000  -0.8282   0.01650   0.01102  -0.0361   0.9586   0.0077
  -9.750  -0.7750   0.01564   0.01008  -0.0423   0.9425   0.0079
  -9.500  -0.7285   0.01500   0.00933  -0.0469   0.9175   0.0081
  -9.250  -0.7042   0.01463   0.00882  -0.0466   0.8831   0.0083
  -9.000  -0.6901   0.01434   0.00837  -0.0441   0.8533   0.0084
  -8.750  -0.6770   0.01406   0.00797  -0.0413   0.8288   0.0086
  -8.500  -0.6640   0.01368   0.00750  -0.0386   0.8112   0.0089
  -8.250  -0.6465   0.01337   0.00712  -0.0367   0.7980   0.0091
  -8.000  -0.6278   0.01310   0.00679  -0.0351   0.7864   0.0093
  -7.750  -0.6086   0.01281   0.00644  -0.0335   0.7758   0.0097
  -7.500  -0.5886   0.01253   0.00610  -0.0321   0.7667   0.0100
  -7.250  -0.5676   0.01230   0.00581  -0.0309   0.7582   0.0104
  -7.000  -0.5461   0.01206   0.00552  -0.0297   0.7504   0.0106
  -6.750  -0.5253   0.01178   0.00519  -0.0284   0.7417   0.0112
  -6.500  -0.5037   0.01151   0.00489  -0.0272   0.7346   0.0117
  -6.250  -0.4814   0.01127   0.00462  -0.0262   0.7268   0.0123
  -6.000  -0.4587   0.01106   0.00436  -0.0252   0.7195   0.0131
  -5.750  -0.4354   0.01085   0.00413  -0.0244   0.7115   0.0138
  -5.500  -0.4124   0.01065   0.00390  -0.0234   0.7038   0.0150
  -5.250  -0.3885   0.01045   0.00370  -0.0227   0.6962   0.0170
  -4.750  -0.3395   0.01016   0.00338  -0.0214   0.6814   0.0236
  -4.500  -0.3148   0.01003   0.00324  -0.0208   0.6738   0.0262
  -4.250  -0.2894   0.00992   0.00310  -0.0203   0.6669   0.0280
  -4.000  -0.2644   0.00978   0.00295  -0.0197   0.6593   0.0299
  -3.750  -0.2391   0.00968   0.00282  -0.0192   0.6530   0.0316
  -3.500  -0.2133   0.00956   0.00269  -0.0188   0.6465   0.0332
  -3.250  -0.1881   0.00945   0.00256  -0.0183   0.6397   0.0358
  -3.000  -0.1622   0.00935   0.00245  -0.0179   0.6331   0.0379
  -2.750  -0.1364   0.00925   0.00233  -0.0175   0.6263   0.0399
  -2.500  -0.1108   0.00915   0.00223  -0.0170   0.6202   0.0439
  -2.250  -0.0849   0.00903   0.00213  -0.0166   0.6138   0.0501
  -2.000  -0.0594   0.00893   0.00204  -0.0162   0.6063   0.0604
  -1.750  -0.0344   0.00878   0.00195  -0.0156   0.5969   0.0828
  -1.500  -0.0173   0.00814   0.00169  -0.0137   0.5834   0.2272
  -1.250  -0.0063   0.00714   0.00139  -0.0108   0.5679   0.4346
  -1.000   0.0167   0.00698   0.00132  -0.0099   0.5523   0.4830
  -0.750   0.0414   0.00688   0.00129  -0.0093   0.5404   0.5171
  -0.500   0.0668   0.00680   0.00127  -0.0088   0.5315   0.5425
  -0.250   0.0918   0.00675   0.00126  -0.0082   0.5223   0.5695
   0.000   0.1175   0.00669   0.00126  -0.0077   0.5144   0.5924
   0.250   0.1430   0.00668   0.00127  -0.0072   0.5061   0.6141
   0.500   0.1694   0.00667   0.00128  -0.0069   0.4975   0.6304
   0.750   0.1955   0.00670   0.00131  -0.0065   0.4875   0.6427
   1.000   0.2223   0.00673   0.00133  -0.0063   0.4775   0.6517
   1.250   0.2490   0.00677   0.00135  -0.0061   0.4683   0.6589
   1.750   0.3020   0.00690   0.00142  -0.0056   0.4440   0.6725
   2.000   0.3281   0.00699   0.00147  -0.0052   0.4288   0.6795
   2.250   0.3538   0.00710   0.00153  -0.0049   0.4115   0.6856
   2.500   0.3793   0.00721   0.00160  -0.0044   0.3944   0.6920
   2.750   0.4046   0.00736   0.00168  -0.0040   0.3745   0.6988
   3.000   0.4291   0.00752   0.00177  -0.0034   0.3510   0.7053
   3.250   0.4530   0.00773   0.00189  -0.0027   0.3266   0.7124
   3.500   0.4772   0.00794   0.00202  -0.0021   0.3040   0.7186
   3.750   0.5012   0.00811   0.00214  -0.0014   0.2857   0.7254
   4.000   0.5257   0.00829   0.00227  -0.0009   0.2703   0.7325
   4.250   0.5493   0.00848   0.00241  -0.0002   0.2528   0.7398
   4.500   0.5730   0.00867   0.00255   0.0005   0.2371   0.7476
   4.750   0.5971   0.00883   0.00269   0.0011   0.2252   0.7551
   5.000   0.6210   0.00899   0.00284   0.0018   0.2154   0.7635
   5.250   0.6448   0.00914   0.00298   0.0025   0.2064   0.7721
   5.500   0.6688   0.00927   0.00313   0.0031   0.1994   0.7820
   5.750   0.6924   0.00940   0.00328   0.0038   0.1933   0.7923
   6.250   0.7393   0.00963   0.00358   0.0054   0.1839   0.8170
   6.500   0.7615   0.00977   0.00376   0.0063   0.1768   0.8314
   6.750   0.7836   0.00990   0.00394   0.0074   0.1706   0.8479
   7.000   0.8057   0.01002   0.00412   0.0084   0.1653   0.8676
   7.250   0.8274   0.01018   0.00433   0.0094   0.1585   0.8916
   7.500   0.8534   0.01034   0.00456   0.0095   0.1512   0.9164
   7.750   0.8867   0.01061   0.00485   0.0079   0.1431   0.9377
   8.000   0.9267   0.01097   0.00518   0.0048   0.1326   0.9520
   8.250   0.9668   0.01139   0.00555   0.0015   0.1201   0.9618
   8.500   1.0023   0.01187   0.00596  -0.0008   0.1050   0.9704
   8.750   1.0350   0.01235   0.00638  -0.0026   0.0932   0.9771
   9.000   1.0627   0.01278   0.00677  -0.0032   0.0854   0.9845
   9.250   1.0908   0.01320   0.00717  -0.0039   0.0779   0.9913
   9.500   1.1175   0.01373   0.00765  -0.0044   0.0690   0.9986
   9.750   1.1384   0.01421   0.00810  -0.0037   0.0616   1.0000
  10.000   1.1431   0.01458   0.00845   0.0004   0.0559   1.0000
  10.250   1.1514   0.01494   0.00880   0.0038   0.0527   1.0000
  10.500   1.1616   0.01534   0.00920   0.0066   0.0498   1.0000
  10.750   1.1724   0.01580   0.00967   0.0092   0.0470   1.0000
  11.000   1.1856   0.01622   0.01012   0.0113   0.0455   1.0000
  11.250   1.1988   0.01669   0.01061   0.0132   0.0440   1.0000
  11.500   1.2112   0.01725   0.01119   0.0152   0.0423   1.0000
  11.750   1.2232   0.01787   0.01183   0.0170   0.0404   1.0000
  12.000   1.2369   0.01846   0.01246   0.0185   0.0393   1.0000
  12.250   1.2507   0.01908   0.01312   0.0199   0.0380   1.0000
  12.500   1.2634   0.01979   0.01387   0.0212   0.0365   1.0000
  12.750   1.2747   0.02065   0.01474   0.0226   0.0348   1.0000
  13.000   1.2869   0.02149   0.01562   0.0238   0.0331   1.0000
  13.250   1.2992   0.02237   0.01654   0.0248   0.0315   1.0000
  13.500   1.3099   0.02340   0.01759   0.0259   0.0295   1.0000
  13.750   1.3203   0.02450   0.01872   0.0268   0.0281   1.0000
  14.000   1.3308   0.02563   0.01990   0.0276   0.0270   1.0000
  14.250   1.3401   0.02689   0.02119   0.0284   0.0258   1.0000
  14.500   1.3481   0.02829   0.02263   0.0291   0.0246   1.0000
  14.750   1.3563   0.02972   0.02411   0.0298   0.0239   1.0000
  15.000   1.3639   0.03124   0.02569   0.0303   0.0233   1.0000
  15.250   1.3707   0.03285   0.02736   0.0308   0.0228   1.0000
  15.500   1.3764   0.03461   0.02918   0.0311   0.0223   1.0000
  15.750   1.3807   0.03655   0.03117   0.0314   0.0216   1.0000
  16.000   1.3843   0.03859   0.03329   0.0316   0.0213   1.0000
  16.250   1.3856   0.04094   0.03569   0.0317   0.0208   1.0000
  16.500   1.3867   0.04339   0.03822   0.0317   0.0205   1.0000
  16.750   1.3880   0.04587   0.04078   0.0315   0.0203   1.0000
  17.000   1.3896   0.04840   0.04339   0.0312   0.0200   1.0000
  17.250   1.3900   0.05113   0.04621   0.0308   0.0197   1.0000
  17.500   1.3895   0.05402   0.04918   0.0303   0.0193   1.0000
  17.750   1.3871   0.05721   0.05246   0.0296   0.0192   1.0000
  18.000   1.3830   0.06068   0.05601   0.0287   0.0188   1.0000
  18.250   1.3781   0.06434   0.05976   0.0276   0.0185   1.0000
  18.500   1.3711   0.06834   0.06386   0.0264   0.0183   1.0000
  18.750   1.3623   0.07267   0.06828   0.0250   0.0182   1.0000
  19.000   1.3523   0.07726   0.07297   0.0234   0.0179   1.0000
  19.250   1.3386   0.08248   0.07829   0.0215   0.0176   1.0000
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