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NACA 64(2)-415 (naca642415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 64(2)-415 (naca642415-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.62 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca642415-il-1000000.txt
Download as CSV file: xf-naca642415-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(2)-415                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8389   0.10377   0.10146  -0.0444   1.0000   0.0140
 -17.500  -0.8981   0.08830   0.08575  -0.0534   1.0000   0.0138
 -17.250  -0.9231   0.07967   0.07695  -0.0587   1.0000   0.0138
 -17.000  -0.9353   0.07364   0.07080  -0.0625   1.0000   0.0139
 -16.750  -0.9570   0.06663   0.06363  -0.0665   1.0000   0.0139
 -16.500  -0.9660   0.06182   0.05868  -0.0693   1.0000   0.0140
 -16.250  -0.9764   0.05710   0.05383  -0.0718   1.0000   0.0140
 -16.000  -0.9833   0.05307   0.04966  -0.0738   1.0000   0.0141
 -15.750  -1.0013   0.04808   0.04450  -0.0756   1.0000   0.0143
 -15.500  -1.0117   0.04422   0.04050  -0.0767   1.0000   0.0144
 -15.250  -1.0152   0.04126   0.03745  -0.0774   1.0000   0.0146
 -15.000  -1.0122   0.03907   0.03521  -0.0779   1.0000   0.0148
 -14.750  -1.0094   0.03691   0.03298  -0.0781   1.0000   0.0149
 -14.500  -1.0053   0.03495   0.03095  -0.0782   1.0000   0.0151
 -14.250  -0.9972   0.03347   0.02943  -0.0783   1.0000   0.0153
 -14.000  -0.9919   0.03175   0.02763  -0.0780   1.0000   0.0154
 -13.750  -0.9843   0.03032   0.02614  -0.0777   1.0000   0.0157
 -13.500  -0.9774   0.02889   0.02463  -0.0771   1.0000   0.0159
 -13.250  -0.9701   0.02757   0.02324  -0.0763   1.0000   0.0161
 -13.000  -0.9624   0.02637   0.02196  -0.0753   1.0000   0.0163
 -12.750  -0.9540   0.02533   0.02086  -0.0741   1.0000   0.0166
 -12.500  -0.9467   0.02436   0.01983  -0.0726   1.0000   0.0168
 -12.250  -0.9424   0.02343   0.01882  -0.0704   1.0000   0.0169
 -11.750  -0.9036   0.02100   0.01621  -0.0718   0.9847   0.0177
 -11.500  -0.8722   0.01986   0.01504  -0.0746   0.9766   0.0182
 -11.250  -0.8362   0.01904   0.01418  -0.0777   0.9690   0.0187
 -11.000  -0.8015   0.01828   0.01336  -0.0803   0.9576   0.0192
 -10.750  -0.7720   0.01763   0.01262  -0.0817   0.9417   0.0196
 -10.500  -0.7502   0.01712   0.01199  -0.0814   0.9239   0.0201
 -10.250  -0.7308   0.01669   0.01145  -0.0804   0.9082   0.0205
 -10.000  -0.7101   0.01636   0.01103  -0.0796   0.8949   0.0208
  -9.750  -0.6951   0.01547   0.01004  -0.0781   0.8822   0.0214
  -9.500  -0.6761   0.01491   0.00942  -0.0771   0.8714   0.0220
  -9.250  -0.6545   0.01451   0.00897  -0.0764   0.8610   0.0226
  -9.000  -0.6320   0.01414   0.00854  -0.0759   0.8519   0.0231
  -8.750  -0.6090   0.01379   0.00812  -0.0753   0.8427   0.0238
  -8.500  -0.5854   0.01343   0.00770  -0.0749   0.8343   0.0244
  -8.250  -0.5609   0.01316   0.00735  -0.0746   0.8261   0.0249
  -8.000  -0.5389   0.01256   0.00669  -0.0740   0.8180   0.0259
  -7.750  -0.5149   0.01217   0.00626  -0.0737   0.8100   0.0269
  -7.500  -0.4895   0.01187   0.00593  -0.0735   0.8026   0.0279
  -7.250  -0.4638   0.01160   0.00560  -0.0733   0.7951   0.0288
  -7.000  -0.4377   0.01137   0.00531  -0.0732   0.7883   0.0297
  -6.750  -0.4125   0.01094   0.00484  -0.0731   0.7810   0.0312
  -6.250  -0.3593   0.01044   0.00428  -0.0730   0.7671   0.0346
  -6.000  -0.3323   0.01024   0.00402  -0.0730   0.7598   0.0361
  -5.750  -0.3057   0.00992   0.00369  -0.0730   0.7531   0.0392
  -5.500  -0.2782   0.00973   0.00347  -0.0731   0.7458   0.0418
  -5.250  -0.2510   0.00948   0.00321  -0.0732   0.7394   0.0466
  -5.000  -0.2233   0.00926   0.00299  -0.0734   0.7327   0.0535
  -4.750  -0.1960   0.00900   0.00277  -0.0735   0.7261   0.0675
  -4.500  -0.1685   0.00868   0.00255  -0.0737   0.7199   0.0953
  -4.250  -0.1413   0.00826   0.00232  -0.0740   0.7133   0.1433
  -4.000  -0.1145   0.00772   0.00205  -0.0744   0.7072   0.2235
  -3.750  -0.0876   0.00694   0.00173  -0.0749   0.7010   0.3480
  -3.500  -0.0600   0.00647   0.00159  -0.0754   0.6947   0.4486
  -3.250  -0.0311   0.00638   0.00154  -0.0757   0.6889   0.4795
  -3.000  -0.0020   0.00633   0.00150  -0.0760   0.6825   0.4976
  -2.750   0.0269   0.00632   0.00146  -0.0762   0.6763   0.5118
  -2.500   0.0562   0.00630   0.00144  -0.0765   0.6704   0.5230
  -2.250   0.0853   0.00628   0.00142  -0.0768   0.6644   0.5337
  -2.000   0.1141   0.00630   0.00141  -0.0770   0.6587   0.5473
  -1.750   0.1435   0.00629   0.00142  -0.0773   0.6533   0.5601
  -1.250   0.2014   0.00634   0.00145  -0.0778   0.6421   0.5829
  -1.000   0.2308   0.00635   0.00145  -0.0781   0.6370   0.5881
  -0.750   0.2599   0.00635   0.00144  -0.0784   0.6316   0.5935
  -0.500   0.2887   0.00639   0.00145  -0.0786   0.6264   0.5988
  -0.250   0.3181   0.00639   0.00146  -0.0790   0.6217   0.6036
   0.000   0.3472   0.00642   0.00147  -0.0792   0.6164   0.6080
   0.250   0.3759   0.00645   0.00149  -0.0795   0.6113   0.6128
   0.500   0.4052   0.00646   0.00152  -0.0798   0.6071   0.6178
   0.750   0.4344   0.00650   0.00155  -0.0801   0.6025   0.6226
   1.000   0.4633   0.00652   0.00158  -0.0803   0.5981   0.6277
   1.250   0.4920   0.00658   0.00163  -0.0806   0.5935   0.6333
   1.500   0.5213   0.00660   0.00167  -0.0809   0.5888   0.6390
   1.750   0.5501   0.00663   0.00172  -0.0811   0.5833   0.6447
   2.000   0.5785   0.00671   0.00179  -0.0813   0.5782   0.6506
   2.250   0.6077   0.00673   0.00184  -0.0816   0.5741   0.6565
   2.500   0.6365   0.00676   0.00190  -0.0818   0.5688   0.6625
   2.750   0.6646   0.00684   0.00198  -0.0820   0.5615   0.6689
   3.000   0.6935   0.00686   0.00203  -0.0822   0.5540   0.6751
   3.250   0.7213   0.00694   0.00210  -0.0823   0.5448   0.6816
   3.500   0.7498   0.00699   0.00217  -0.0824   0.5354   0.6885
   3.750   0.7778   0.00706   0.00225  -0.0825   0.5254   0.6950
   4.000   0.8053   0.00716   0.00234  -0.0825   0.5130   0.7022
   4.250   0.8335   0.00724   0.00244  -0.0827   0.5029   0.7093
   4.500   0.8612   0.00732   0.00256  -0.0827   0.4932   0.7166
   4.750   0.8885   0.00746   0.00268  -0.0827   0.4802   0.7240
   5.000   0.9155   0.00759   0.00282  -0.0827   0.4644   0.7311
   5.250   0.9415   0.00781   0.00298  -0.0824   0.4385   0.7388
   5.500   0.9611   0.00848   0.00333  -0.0813   0.3642   0.7460
   5.750   0.9766   0.00950   0.00393  -0.0795   0.2794   0.7539
   6.000   0.9931   0.01040   0.00450  -0.0779   0.2096   0.7616
   6.250   1.0107   0.01117   0.00502  -0.0765   0.1590   0.7698
   6.500   1.0289   0.01185   0.00551  -0.0752   0.1185   0.7779
   6.750   1.0473   0.01247   0.00599  -0.0738   0.0889   0.7868
   7.000   1.0662   0.01302   0.00645  -0.0725   0.0676   0.7957
   7.250   1.0852   0.01353   0.00690  -0.0713   0.0527   0.8053
   7.500   1.1041   0.01399   0.00735  -0.0700   0.0434   0.8146
   8.000   1.1401   0.01489   0.00826  -0.0670   0.0338   0.8348
   8.250   1.1563   0.01524   0.00867  -0.0652   0.0316   0.8458
   8.500   1.1700   0.01568   0.00915  -0.0629   0.0294   0.8587
   8.750   1.1818   0.01619   0.00972  -0.0604   0.0273   0.8737
   9.000   1.1952   0.01659   0.01021  -0.0581   0.0258   0.8915
   9.250   1.2049   0.01709   0.01078  -0.0554   0.0243   0.9166
   9.500   1.2113   0.01767   0.01149  -0.0522   0.0229   1.0000
   9.750   1.2278   0.01825   0.01211  -0.0510   0.0219   1.0000
  10.000   1.2423   0.01895   0.01282  -0.0497   0.0209   1.0000
  10.250   1.2552   0.01977   0.01366  -0.0482   0.0199   1.0000
  10.500   1.2630   0.02093   0.01485  -0.0462   0.0189   1.0000
  10.750   1.2771   0.02174   0.01571  -0.0451   0.0184   1.0000
  11.000   1.2900   0.02265   0.01666  -0.0438   0.0178   1.0000
  11.250   1.3024   0.02362   0.01767  -0.0426   0.0173   1.0000
  11.500   1.3142   0.02467   0.01875  -0.0415   0.0168   1.0000
  11.750   1.3239   0.02590   0.02001  -0.0402   0.0163   1.0000
  12.000   1.3291   0.02752   0.02168  -0.0387   0.0158   1.0000
  12.250   1.3331   0.02930   0.02353  -0.0373   0.0154   1.0000
  12.500   1.3453   0.03046   0.02475  -0.0365   0.0152   1.0000
  12.750   1.3542   0.03194   0.02629  -0.0356   0.0150   1.0000
  13.000   1.3646   0.03332   0.02771  -0.0349   0.0146   1.0000
  13.250   1.3734   0.03486   0.02932  -0.0341   0.0143   1.0000
  13.500   1.3817   0.03649   0.03100  -0.0334   0.0140   1.0000
  13.750   1.3892   0.03823   0.03279  -0.0328   0.0138   1.0000
  14.000   1.3960   0.04009   0.03471  -0.0323   0.0136   1.0000
  14.250   1.4022   0.04204   0.03671  -0.0318   0.0134   1.0000
  14.500   1.4069   0.04422   0.03895  -0.0314   0.0131   1.0000
  14.750   1.4094   0.04669   0.04148  -0.0310   0.0129   1.0000
  15.000   1.4090   0.04954   0.04441  -0.0308   0.0127   1.0000
  15.250   1.4042   0.05296   0.04793  -0.0305   0.0125   1.0000
  15.500   1.4087   0.05546   0.05051  -0.0306   0.0124   1.0000
  15.750   1.4145   0.05784   0.05298  -0.0307   0.0123   1.0000
  16.000   1.4186   0.06048   0.05570  -0.0310   0.0122   1.0000
  16.250   1.4211   0.06339   0.05869  -0.0314   0.0121   1.0000
  16.500   1.4239   0.06633   0.06172  -0.0318   0.0120   1.0000
  16.750   1.4261   0.06940   0.06488  -0.0324   0.0119   1.0000
  17.000   1.4270   0.07272   0.06829  -0.0331   0.0118   1.0000
  17.250   1.4270   0.07622   0.07188  -0.0340   0.0117   1.0000
  17.500   1.4271   0.07979   0.07556  -0.0350   0.0116   1.0000
  17.750   1.4267   0.08351   0.07938  -0.0361   0.0115   1.0000
  18.000   1.4247   0.08753   0.08349  -0.0375   0.0114   1.0000
  18.250   1.4227   0.09165   0.08771  -0.0389   0.0113   1.0000
  18.500   1.4204   0.09590   0.09206  -0.0406   0.0112   1.0000
  18.750   1.4172   0.10036   0.09662  -0.0424   0.0111   1.0000
  19.000   1.4133   0.10501   0.10138  -0.0444   0.0110   1.0000
  19.250   1.4092   0.10979   0.10625  -0.0467   0.0109   1.0000
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