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NACA 64A410 (naca64a410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64A410 (naca64a410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.9 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca64a410-il-1000000-n5.txt
Download as CSV file: xf-naca64a410-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64A410                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4812   0.13305   0.13132  -0.0188   1.0000   0.0039
 -12.250  -0.4784   0.12882   0.12710  -0.0205   1.0000   0.0040
 -11.250  -0.7945   0.02995   0.02738  -0.0830   0.9771   0.0046
 -11.000  -0.7858   0.02547   0.02242  -0.0840   0.9666   0.0047
 -10.750  -0.7694   0.02313   0.01977  -0.0841   0.9591   0.0048
 -10.500  -0.7503   0.02141   0.01780  -0.0840   0.9525   0.0049
 -10.250  -0.7321   0.01945   0.01554  -0.0838   0.9466   0.0051
 -10.000  -0.7105   0.01821   0.01412  -0.0836   0.9413   0.0053
  -9.750  -0.6869   0.01741   0.01320  -0.0834   0.9368   0.0055
  -9.500  -0.6625   0.01674   0.01243  -0.0834   0.9324   0.0057
  -9.250  -0.6377   0.01613   0.01171  -0.0833   0.9278   0.0059
  -9.000  -0.6129   0.01551   0.01098  -0.0831   0.9236   0.0061
  -8.750  -0.5879   0.01489   0.01024  -0.0830   0.9196   0.0064
  -8.500  -0.5627   0.01427   0.00950  -0.0829   0.9148   0.0067
  -8.250  -0.5374   0.01370   0.00882  -0.0828   0.9099   0.0070
  -8.000  -0.5116   0.01323   0.00823  -0.0827   0.9055   0.0072
  -7.750  -0.4860   0.01263   0.00753  -0.0826   0.9010   0.0076
  -7.500  -0.4596   0.01226   0.00711  -0.0826   0.8967   0.0081
  -7.000  -0.4062   0.01160   0.00635  -0.0826   0.8889   0.0089
  -6.750  -0.3795   0.01123   0.00591  -0.0826   0.8846   0.0094
  -6.500  -0.3528   0.01088   0.00548  -0.0825   0.8805   0.0098
  -6.250  -0.3259   0.01058   0.00510  -0.0825   0.8766   0.0102
  -6.000  -0.2990   0.01022   0.00469  -0.0825   0.8721   0.0106
  -5.750  -0.2726   0.00979   0.00421  -0.0824   0.8675   0.0115
  -5.500  -0.2456   0.00957   0.00395  -0.0824   0.8621   0.0122
  -5.250  -0.2186   0.00931   0.00364  -0.0823   0.8538   0.0128
  -5.000  -0.1917   0.00907   0.00333  -0.0823   0.8463   0.0134
  -4.750  -0.1643   0.00885   0.00306  -0.0823   0.8398   0.0140
  -4.500  -0.1370   0.00868   0.00283  -0.0822   0.8335   0.0145
  -4.250  -0.1098   0.00837   0.00247  -0.0822   0.8260   0.0157
  -4.000  -0.0825   0.00817   0.00223  -0.0822   0.8178   0.0168
  -3.750  -0.0551   0.00801   0.00203  -0.0822   0.8078   0.0179
  -3.500  -0.0276   0.00787   0.00184  -0.0821   0.7973   0.0193
  -3.250  -0.0003   0.00774   0.00166  -0.0821   0.7858   0.0218
  -3.000   0.0268   0.00764   0.00153  -0.0820   0.7723   0.0262
  -2.750   0.0539   0.00756   0.00140  -0.0819   0.7571   0.0316
  -2.500   0.0809   0.00751   0.00129  -0.0818   0.7425   0.0370
  -2.250   0.1081   0.00746   0.00119  -0.0817   0.7283   0.0435
  -2.000   0.1351   0.00744   0.00111  -0.0816   0.7118   0.0490
  -1.500   0.1894   0.00727   0.00101  -0.0815   0.6874   0.1029
  -1.250   0.2169   0.00729   0.00098  -0.0815   0.6749   0.1080
  -1.000   0.2444   0.00729   0.00094  -0.0815   0.6611   0.1122
  -0.750   0.2716   0.00730   0.00090  -0.0815   0.6457   0.1165
  -0.500   0.2988   0.00733   0.00089  -0.0814   0.6298   0.1202
  -0.250   0.3261   0.00737   0.00088  -0.0813   0.6148   0.1240
   0.000   0.3532   0.00740   0.00088  -0.0813   0.5989   0.1316
   0.250   0.3773   0.00658   0.00084  -0.0813   0.5827   0.4293
   0.500   0.4035   0.00645   0.00088  -0.0811   0.5649   0.5091
   0.750   0.4299   0.00644   0.00094  -0.0810   0.5456   0.5591
   1.000   0.4553   0.00664   0.00103  -0.0807   0.5050   0.5816
   1.250   0.4783   0.00709   0.00120  -0.0800   0.4245   0.6008
   1.500   0.4904   0.00885   0.00182  -0.0777   0.1376   0.6157
   1.750   0.5170   0.00899   0.00194  -0.0776   0.1230   0.6328
   2.000   0.5440   0.00907   0.00205  -0.0776   0.1191   0.6497
   2.250   0.5709   0.00918   0.00217  -0.0775   0.1138   0.6663
   2.500   0.5978   0.00926   0.00230  -0.0774   0.1103   0.6851
   2.750   0.6248   0.00934   0.00243  -0.0773   0.1092   0.7022
   3.000   0.6517   0.00943   0.00257  -0.0773   0.1064   0.7169
   3.250   0.6780   0.00959   0.00273  -0.0771   0.0995   0.7318
   3.500   0.7047   0.00970   0.00288  -0.0770   0.0959   0.7466
   3.750   0.7314   0.00980   0.00302  -0.0769   0.0894   0.7609
   4.000   0.7557   0.01016   0.00323  -0.0765   0.0514   0.7754
   4.250   0.7813   0.01035   0.00345  -0.0762   0.0441   0.7911
   4.500   0.8068   0.01050   0.00367  -0.0759   0.0390   0.8092
   4.750   0.8314   0.01062   0.00391  -0.0753   0.0338   0.8406
   5.000   0.8595   0.01064   0.00416  -0.0755   0.0270   1.0000
   5.250   0.8844   0.01095   0.00442  -0.0751   0.0204   1.0000
   5.500   0.9091   0.01126   0.00470  -0.0747   0.0162   1.0000
   5.750   0.9340   0.01155   0.00500  -0.0743   0.0143   1.0000
   6.000   0.9587   0.01185   0.00531  -0.0739   0.0132   1.0000
   6.250   0.9831   0.01218   0.00565  -0.0735   0.0123   1.0000
   6.500   1.0071   0.01255   0.00603  -0.0729   0.0115   1.0000
   6.750   1.0304   0.01298   0.00650  -0.0723   0.0109   1.0000
   7.000   1.0536   0.01339   0.00695  -0.0717   0.0106   1.0000
   7.250   1.0770   0.01378   0.00738  -0.0710   0.0104   1.0000
   7.500   1.0999   0.01421   0.00785  -0.0704   0.0101   1.0000
   7.750   1.1225   0.01464   0.00832  -0.0697   0.0098   1.0000
   8.000   1.1448   0.01509   0.00882  -0.0689   0.0094   1.0000
   8.250   1.1664   0.01558   0.00936  -0.0681   0.0092   1.0000
   8.500   1.1875   0.01610   0.00993  -0.0672   0.0089   1.0000
   8.750   1.2081   0.01665   0.01052  -0.0662   0.0087   1.0000
   9.000   1.2283   0.01721   0.01112  -0.0652   0.0084   1.0000
   9.250   1.2479   0.01779   0.01175  -0.0641   0.0081   1.0000
   9.500   1.2656   0.01851   0.01254  -0.0627   0.0078   1.0000
   9.750   1.2790   0.01949   0.01360  -0.0606   0.0075   1.0000
  10.000   1.2928   0.02039   0.01459  -0.0586   0.0073   1.0000
  10.250   1.3092   0.02103   0.01530  -0.0570   0.0072   1.0000
  10.500   1.3250   0.02171   0.01605  -0.0554   0.0071   1.0000
  10.750   1.3405   0.02241   0.01683  -0.0539   0.0070   1.0000
  11.000   1.3558   0.02311   0.01760  -0.0523   0.0068   1.0000
  11.250   1.3706   0.02385   0.01843  -0.0508   0.0066   1.0000
  11.500   1.3844   0.02467   0.01932  -0.0492   0.0064   1.0000
  11.750   1.3980   0.02550   0.02023  -0.0477   0.0062   1.0000
  12.000   1.4106   0.02642   0.02123  -0.0461   0.0060   1.0000
  12.250   1.4229   0.02736   0.02224  -0.0445   0.0058   1.0000
  12.500   1.4347   0.02836   0.02331  -0.0430   0.0057   1.0000
  12.750   1.4462   0.02939   0.02441  -0.0416   0.0055   1.0000
  13.000   1.4568   0.03050   0.02559  -0.0401   0.0054   1.0000
  13.250   1.4658   0.03178   0.02695  -0.0386   0.0052   1.0000
  13.500   1.4717   0.03336   0.02864  -0.0369   0.0051   1.0000
  13.750   1.4714   0.03557   0.03098  -0.0350   0.0049   1.0000
  14.000   1.4777   0.03721   0.03273  -0.0336   0.0049   1.0000
  14.250   1.4829   0.03898   0.03462  -0.0324   0.0048   1.0000
  14.500   1.4878   0.04084   0.03659  -0.0313   0.0047   1.0000
  14.750   1.4911   0.04291   0.03878  -0.0304   0.0046   1.0000
  15.000   1.4938   0.04510   0.04109  -0.0295   0.0045   1.0000
  15.250   1.4945   0.04758   0.04370  -0.0288   0.0044   1.0000
  15.500   1.4945   0.05023   0.04647  -0.0283   0.0043   1.0000
  15.750   1.4926   0.05317   0.04952  -0.0280   0.0042   1.0000
  16.000   1.4915   0.05614   0.05261  -0.0280   0.0041   1.0000
  16.250   1.4885   0.05952   0.05611  -0.0282   0.0040   1.0000
  16.500   1.4836   0.06327   0.05998  -0.0287   0.0039   1.0000
  16.750   1.4781   0.06726   0.06410  -0.0295   0.0038   1.0000
  17.000   1.4704   0.07176   0.06872  -0.0306   0.0038   1.0000
  17.250   1.4611   0.07669   0.07378  -0.0322   0.0037   1.0000
  17.500   1.4478   0.08244   0.07967  -0.0343   0.0037   1.0000
  17.750   1.4311   0.08906   0.08644  -0.0370   0.0036   1.0000
  18.000   1.4085   0.09713   0.09467  -0.0407   0.0036   1.0000
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