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NACA 64(2)-415 (naca642415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(2)-415 (naca642415-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.14 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca642415-il-1000000-n5.txt
Download as CSV file: xf-naca642415-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.9114   0.12058   0.11809  -0.0342   1.0000   0.0107
 -19.250  -0.9623   0.10698   0.10431  -0.0416   1.0000   0.0106
 -19.000  -1.0042   0.09538   0.09253  -0.0480   1.0000   0.0106
 -18.750  -1.0358   0.08597   0.08297  -0.0533   1.0000   0.0106
 -18.500  -1.0593   0.07827   0.07512  -0.0576   1.0000   0.0106
 -18.250  -1.0749   0.07205   0.06877  -0.0611   1.0000   0.0107
 -18.000  -1.0920   0.06590   0.06249  -0.0645   1.0000   0.0106
 -17.750  -1.1042   0.06081   0.05729  -0.0672   1.0000   0.0108
 -17.500  -1.1140   0.05622   0.05260  -0.0694   1.0000   0.0109
 -17.250  -1.1203   0.05230   0.04858  -0.0713   1.0000   0.0110
 -17.000  -1.1231   0.04896   0.04515  -0.0727   1.0000   0.0111
 -16.750  -1.1245   0.04595   0.04206  -0.0738   1.0000   0.0112
 -16.500  -1.1235   0.04334   0.03937  -0.0746   1.0000   0.0114
 -16.250  -1.1220   0.04085   0.03680  -0.0753   1.0000   0.0115
 -16.000  -1.1188   0.03860   0.03449  -0.0758   1.0000   0.0116
 -15.750  -1.1141   0.03657   0.03238  -0.0762   1.0000   0.0117
 -15.500  -1.1084   0.03468   0.03043  -0.0764   1.0000   0.0119
 -15.250  -1.1015   0.03297   0.02865  -0.0764   1.0000   0.0120
 -15.000  -1.0939   0.03136   0.02697  -0.0764   1.0000   0.0122
 -14.750  -1.0860   0.02984   0.02539  -0.0762   1.0000   0.0124
 -14.500  -1.0780   0.02839   0.02386  -0.0758   1.0000   0.0125
 -14.250  -1.0692   0.02706   0.02247  -0.0754   1.0000   0.0127
 -14.000  -1.0595   0.02586   0.02121  -0.0748   1.0000   0.0129
 -13.750  -1.0493   0.02477   0.02006  -0.0741   1.0000   0.0130
 -13.500  -1.0374   0.02388   0.01911  -0.0732   1.0000   0.0132
 -13.250  -1.0294   0.02280   0.01797  -0.0720   1.0000   0.0134
 -13.000  -1.0171   0.02165   0.01677  -0.0716   0.9867   0.0136
 -12.750  -0.9806   0.02055   0.01562  -0.0756   0.9733   0.0140
 -12.500  -0.9401   0.01957   0.01457  -0.0802   0.9586   0.0143
 -12.250  -0.9050   0.01875   0.01367  -0.0833   0.9372   0.0147
 -12.000  -0.8865   0.01814   0.01292  -0.0830   0.9119   0.0149
 -11.750  -0.8768   0.01760   0.01226  -0.0808   0.8909   0.0151
 -11.500  -0.8634   0.01715   0.01171  -0.0791   0.8756   0.0154
 -11.000  -0.8274   0.01627   0.01065  -0.0769   0.8519   0.0159
 -10.750  -0.8077   0.01588   0.01016  -0.0760   0.8421   0.0162
 -10.500  -0.7881   0.01540   0.00962  -0.0752   0.8319   0.0166
 -10.250  -0.7675   0.01495   0.00911  -0.0744   0.8231   0.0170
 -10.000  -0.7457   0.01456   0.00866  -0.0738   0.8140   0.0174
  -9.750  -0.7229   0.01420   0.00826  -0.0734   0.8060   0.0178
  -9.500  -0.6996   0.01387   0.00787  -0.0729   0.7970   0.0182
  -9.250  -0.6757   0.01356   0.00750  -0.0726   0.7891   0.0187
  -9.000  -0.6514   0.01326   0.00714  -0.0723   0.7804   0.0192
  -8.750  -0.6267   0.01297   0.00678  -0.0720   0.7729   0.0196
  -8.500  -0.6022   0.01263   0.00639  -0.0718   0.7650   0.0201
  -8.250  -0.5774   0.01231   0.00603  -0.0716   0.7578   0.0207
  -8.000  -0.5517   0.01203   0.00572  -0.0715   0.7504   0.0214
  -7.750  -0.5260   0.01178   0.00542  -0.0713   0.7432   0.0221
  -7.500  -0.4995   0.01154   0.00515  -0.0713   0.7363   0.0228
  -7.250  -0.4730   0.01134   0.00489  -0.0713   0.7295   0.0236
  -7.000  -0.4466   0.01107   0.00460  -0.0713   0.7234   0.0246
  -6.750  -0.4198   0.01084   0.00434  -0.0713   0.7168   0.0257
  -6.250  -0.3654   0.01046   0.00389  -0.0715   0.7045   0.0279
  -6.000  -0.3381   0.01027   0.00367  -0.0715   0.6978   0.0292
  -5.750  -0.3107   0.01007   0.00345  -0.0716   0.6915   0.0311
  -5.500  -0.2830   0.00991   0.00326  -0.0718   0.6850   0.0330
  -5.250  -0.2553   0.00975   0.00308  -0.0719   0.6786   0.0355
  -5.000  -0.2274   0.00957   0.00290  -0.0721   0.6732   0.0388
  -4.750  -0.1993   0.00941   0.00274  -0.0723   0.6673   0.0429
  -4.500  -0.1714   0.00926   0.00258  -0.0725   0.6616   0.0492
  -4.250  -0.1433   0.00907   0.00243  -0.0727   0.6565   0.0599
  -4.000  -0.1151   0.00887   0.00227  -0.0730   0.6508   0.0759
  -3.750  -0.0872   0.00866   0.00213  -0.0732   0.6453   0.0971
  -3.500  -0.0590   0.00839   0.00197  -0.0736   0.6404   0.1319
  -3.250  -0.0308   0.00807   0.00181  -0.0740   0.6349   0.1790
  -3.000  -0.0029   0.00768   0.00163  -0.0744   0.6295   0.2456
  -2.750   0.0251   0.00721   0.00144  -0.0749   0.6245   0.3295
  -2.500   0.0535   0.00679   0.00130  -0.0755   0.6190   0.4148
  -2.250   0.0823   0.00667   0.00126  -0.0758   0.6133   0.4565
  -2.000   0.1113   0.00659   0.00124  -0.0762   0.6085   0.4839
  -1.750   0.1405   0.00653   0.00124  -0.0765   0.6036   0.5083
  -1.500   0.1695   0.00649   0.00125  -0.0768   0.5986   0.5313
  -1.250   0.1985   0.00650   0.00125  -0.0771   0.5942   0.5427
  -1.000   0.2278   0.00649   0.00125  -0.0774   0.5900   0.5485
  -0.750   0.2570   0.00651   0.00125  -0.0777   0.5855   0.5542
  -0.500   0.2861   0.00653   0.00125  -0.0779   0.5811   0.5588
  -0.250   0.3152   0.00655   0.00126  -0.0782   0.5773   0.5628
   0.000   0.3444   0.00656   0.00128  -0.0785   0.5736   0.5667
   0.250   0.3736   0.00659   0.00130  -0.0788   0.5694   0.5706
   0.500   0.4025   0.00663   0.00132  -0.0791   0.5652   0.5743
   0.750   0.4315   0.00666   0.00135  -0.0794   0.5614   0.5789
   1.000   0.4607   0.00667   0.00139  -0.0797   0.5580   0.5837
   1.250   0.4898   0.00671   0.00143  -0.0799   0.5539   0.5882
   1.500   0.5185   0.00676   0.00148  -0.0802   0.5492   0.5923
   1.750   0.5473   0.00680   0.00153  -0.0804   0.5445   0.5971
   2.000   0.5763   0.00683   0.00158  -0.0807   0.5397   0.6020
   2.250   0.6051   0.00689   0.00164  -0.0809   0.5348   0.6067
   2.500   0.6335   0.00695   0.00171  -0.0811   0.5291   0.6115
   2.750   0.6621   0.00700   0.00178  -0.0813   0.5199   0.6170
   3.000   0.6902   0.00709   0.00185  -0.0814   0.5094   0.6222
   3.250   0.7178   0.00721   0.00194  -0.0815   0.4952   0.6273
   3.500   0.7452   0.00734   0.00204  -0.0815   0.4775   0.6334
   3.750   0.7725   0.00749   0.00215  -0.0815   0.4596   0.6395
   4.000   0.7983   0.00774   0.00230  -0.0813   0.4266   0.6455
   4.250   0.8190   0.00842   0.00264  -0.0803   0.3522   0.6519
   4.500   0.8412   0.00898   0.00298  -0.0796   0.3022   0.6578
   4.750   0.8630   0.00955   0.00335  -0.0788   0.2520   0.6638
   5.000   0.8841   0.01016   0.00375  -0.0779   0.2033   0.6703
   5.500   0.9273   0.01123   0.00449  -0.0763   0.1294   0.6830
   5.750   0.9480   0.01179   0.00490  -0.0753   0.0973   0.6899
   6.000   0.9692   0.01228   0.00529  -0.0744   0.0734   0.6962
   6.250   0.9908   0.01272   0.00565  -0.0736   0.0565   0.7034
   6.750   1.0350   0.01346   0.00635  -0.0721   0.0392   0.7179
   7.000   1.0571   0.01380   0.00669  -0.0713   0.0345   0.7260
   7.250   1.0787   0.01414   0.00705  -0.0704   0.0310   0.7337
   7.500   1.1000   0.01448   0.00741  -0.0695   0.0284   0.7418
   7.750   1.1203   0.01484   0.00779  -0.0685   0.0262   0.7493
   8.000   1.1401   0.01517   0.00816  -0.0673   0.0247   0.7576
   8.250   1.1566   0.01554   0.00856  -0.0655   0.0231   0.7656
   8.500   1.1724   0.01594   0.00900  -0.0637   0.0218   0.7749
   8.750   1.1887   0.01633   0.00944  -0.0620   0.0207   0.7847
   9.250   1.2180   0.01730   0.01050  -0.0583   0.0182   0.8064
   9.500   1.2331   0.01780   0.01106  -0.0567   0.0174   0.8176
   9.750   1.2473   0.01835   0.01167  -0.0550   0.0162   0.8304
  10.000   1.2606   0.01897   0.01234  -0.0533   0.0155   0.8445
  10.250   1.2730   0.01963   0.01308  -0.0515   0.0147   0.8601
  10.500   1.2853   0.02029   0.01384  -0.0497   0.0141   0.8800
  10.750   1.2956   0.02096   0.01462  -0.0476   0.0137   0.9093
  11.000   1.3063   0.02164   0.01543  -0.0457   0.0131   1.0000
  11.250   1.3191   0.02255   0.01636  -0.0445   0.0127   1.0000
  11.500   1.3306   0.02358   0.01743  -0.0432   0.0121   1.0000
  11.750   1.3427   0.02461   0.01849  -0.0421   0.0118   1.0000
  12.000   1.3548   0.02567   0.01959  -0.0411   0.0116   1.0000
  12.250   1.3664   0.02678   0.02075  -0.0401   0.0113   1.0000
  12.500   1.3774   0.02798   0.02200  -0.0391   0.0111   1.0000
  12.750   1.3882   0.02923   0.02330  -0.0381   0.0109   1.0000
  13.000   1.3983   0.03056   0.02467  -0.0373   0.0107   1.0000
  13.250   1.4079   0.03197   0.02613  -0.0364   0.0105   1.0000
  13.500   1.4169   0.03346   0.02766  -0.0356   0.0104   1.0000
  13.750   1.4252   0.03504   0.02929  -0.0349   0.0102   1.0000
  14.000   1.4330   0.03671   0.03101  -0.0342   0.0100   1.0000
  14.250   1.4395   0.03855   0.03290  -0.0336   0.0098   1.0000
  14.500   1.4448   0.04054   0.03497  -0.0330   0.0096   1.0000
  14.750   1.4493   0.04269   0.03718  -0.0325   0.0095   1.0000
  15.000   1.4564   0.04464   0.03919  -0.0322   0.0095   1.0000
  15.250   1.4626   0.04671   0.04133  -0.0320   0.0094   1.0000
  15.500   1.4679   0.04893   0.04363  -0.0318   0.0094   1.0000
  15.750   1.4726   0.05129   0.04606  -0.0317   0.0093   1.0000
  16.000   1.4773   0.05369   0.04854  -0.0318   0.0092   1.0000
  16.250   1.4816   0.05621   0.05114  -0.0319   0.0091   1.0000
  16.500   1.4846   0.05894   0.05395  -0.0322   0.0091   1.0000
  16.750   1.4878   0.06171   0.05680  -0.0325   0.0090   1.0000
  17.000   1.4911   0.06451   0.05968  -0.0329   0.0089   1.0000
  17.250   1.4928   0.06760   0.06286  -0.0335   0.0088   1.0000
  17.500   1.4935   0.07089   0.06622  -0.0343   0.0087   1.0000
  17.750   1.4929   0.07441   0.06984  -0.0351   0.0086   1.0000
  18.000   1.4930   0.07792   0.07344  -0.0361   0.0085   1.0000
  18.250   1.4916   0.08173   0.07733  -0.0372   0.0085   1.0000
  18.500   1.4892   0.08578   0.08148  -0.0386   0.0084   1.0000
  18.750   1.4866   0.08991   0.08572  -0.0401   0.0084   1.0000
  19.000   1.4828   0.09433   0.09023  -0.0417   0.0083   1.0000
  19.250   1.4779   0.09902   0.09503  -0.0437   0.0083   1.0000
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