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NACA 0010-65 (naca001065-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0010-65 (naca001065-il)
Reynolds number: 1,000,000
Max Cl/Cd: 57.44 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca001065-il-1000000.txt
Download as CSV file: xf-naca001065-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-65                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0187   0.09102   0.08900  -0.0346   1.0000   0.0095
 -16.250  -1.1350   0.05932   0.05687  -0.0560   1.0000   0.0090
 -16.000  -1.1656   0.05126   0.04859  -0.0604   1.0000   0.0090
 -15.750  -1.1845   0.04628   0.04342  -0.0613   1.0000   0.0090
 -15.500  -1.1965   0.04271   0.03969  -0.0609   1.0000   0.0091
 -15.250  -1.2051   0.03982   0.03663  -0.0596   1.0000   0.0092
 -15.000  -1.2088   0.03760   0.03427  -0.0578   1.0000   0.0092
 -14.750  -1.2090   0.03582   0.03235  -0.0559   1.0000   0.0093
 -14.500  -1.2152   0.03368   0.03005  -0.0530   1.0000   0.0094
 -14.250  -1.2337   0.03086   0.02698  -0.0482   1.0000   0.0097
 -14.000  -1.2404   0.02916   0.02514  -0.0439   1.0000   0.0099
 -13.750  -1.2410   0.02805   0.02393  -0.0400   1.0000   0.0101
 -13.500  -1.2397   0.02721   0.02302  -0.0360   1.0000   0.0103
 -13.250  -1.2385   0.02656   0.02230  -0.0317   1.0000   0.0105
 -13.000  -1.2398   0.02602   0.02169  -0.0267   1.0000   0.0107
 -12.750  -1.2424   0.02553   0.02113  -0.0213   1.0000   0.0109
 -12.500  -1.2388   0.02494   0.02046  -0.0171   1.0000   0.0112
 -12.250  -1.2329   0.02433   0.01976  -0.0134   1.0000   0.0114
 -12.000  -1.2259   0.02369   0.01901  -0.0098   1.0000   0.0117
 -11.750  -1.2174   0.02307   0.01830  -0.0065   1.0000   0.0120
 -11.500  -1.2072   0.02251   0.01763  -0.0034   1.0000   0.0122
 -11.250  -1.1943   0.02154   0.01652  -0.0011   0.9997   0.0126
 -11.000  -1.1728   0.02043   0.01533  -0.0007   0.9987   0.0133
 -10.750  -1.1457   0.02004   0.01491  -0.0012   0.9977   0.0138
 -10.500  -1.1179   0.01973   0.01456  -0.0017   0.9967   0.0144
 -10.250  -1.0899   0.01940   0.01418  -0.0023   0.9959   0.0151
 -10.000  -1.0617   0.01909   0.01380  -0.0029   0.9951   0.0157
  -9.750  -1.0352   0.01839   0.01298  -0.0032   0.9945   0.0163
  -9.500  -1.0113   0.01762   0.01218  -0.0030   0.9934   0.0172
  -9.250  -0.9851   0.01739   0.01193  -0.0031   0.9918   0.0179
  -9.000  -0.9579   0.01713   0.01165  -0.0033   0.9904   0.0186
  -8.750  -0.9303   0.01683   0.01130  -0.0037   0.9891   0.0195
  -8.500  -0.9012   0.01668   0.01110  -0.0043   0.9880   0.0202
  -8.250  -0.8749   0.01586   0.01019  -0.0045   0.9870   0.0212
  -8.000  -0.8467   0.01533   0.00964  -0.0051   0.9861   0.0222
  -7.750  -0.8168   0.01503   0.00934  -0.0059   0.9853   0.0232
  -7.500  -0.7867   0.01473   0.00901  -0.0068   0.9847   0.0242
  -7.250  -0.7559   0.01448   0.00873  -0.0078   0.9841   0.0252
  -7.000  -0.7240   0.01433   0.00854  -0.0090   0.9836   0.0259
  -6.750  -0.7052   0.01373   0.00788  -0.0073   0.9804   0.0266
  -6.500  -0.6824   0.01295   0.00705  -0.0065   0.9783   0.0281
  -6.250  -0.6544   0.01260   0.00670  -0.0069   0.9768   0.0292
  -6.000  -0.6251   0.01228   0.00637  -0.0075   0.9756   0.0304
  -5.750  -0.5954   0.01195   0.00601  -0.0082   0.9746   0.0314
  -5.500  -0.5647   0.01167   0.00571  -0.0091   0.9738   0.0324
  -5.250  -0.5332   0.01143   0.00545  -0.0101   0.9731   0.0331
  -5.000  -0.5027   0.01098   0.00495  -0.0110   0.9725   0.0343
  -4.750  -0.4715   0.01059   0.00454  -0.0119   0.9719   0.0363
  -4.500  -0.4393   0.01031   0.00427  -0.0132   0.9714   0.0383
  -4.250  -0.4071   0.01008   0.00403  -0.0143   0.9709   0.0402
  -4.000  -0.3919   0.00994   0.00388  -0.0115   0.9656   0.0415
  -3.750  -0.3632   0.00968   0.00363  -0.0119   0.9639   0.0463
  -3.500  -0.3342   0.00938   0.00343  -0.0123   0.9624   0.0604
  -3.250  -0.3051   0.00906   0.00324  -0.0128   0.9611   0.0899
  -3.000  -0.2759   0.00873   0.00307  -0.0134   0.9599   0.1242
  -2.750  -0.2471   0.00840   0.00291  -0.0139   0.9588   0.1677
  -2.500  -0.2188   0.00802   0.00276  -0.0142   0.9576   0.2263
  -2.250  -0.2021   0.00761   0.00266  -0.0120   0.9533   0.3082
  -2.000  -0.1866   0.00687   0.00246  -0.0097   0.9493   0.4573
  -1.750  -0.1764   0.00582   0.00218  -0.0061   0.9459   0.6643
  -1.500  -0.1576   0.00531   0.00209  -0.0039   0.9437   0.7748
  -1.250  -0.1362   0.00517   0.00213  -0.0023   0.9405   0.8257
  -1.000  -0.1127   0.00512   0.00217  -0.0012   0.9369   0.8557
  -0.750  -0.0840   0.00502   0.00214  -0.0011   0.9334   0.8768
  -0.500  -0.0512   0.00485   0.00198  -0.0018   0.9284   0.8910
  -0.250  -0.0277   0.00483   0.00197  -0.0004   0.9206   0.9032
   0.000   0.0000   0.00479   0.00192   0.0000   0.9140   0.9140
   0.250   0.0278   0.00483   0.00198   0.0004   0.9032   0.9206
   0.500   0.0513   0.00485   0.00198   0.0017   0.8912   0.9283
   0.750   0.0840   0.00502   0.00214   0.0011   0.8769   0.9334
   1.000   0.1127   0.00512   0.00217   0.0012   0.8557   0.9369
   1.250   0.1362   0.00517   0.00213   0.0023   0.8254   0.9405
   1.500   0.1577   0.00530   0.00209   0.0039   0.7753   0.9437
   1.750   0.1767   0.00581   0.00218   0.0060   0.6667   0.9459
   2.000   0.1868   0.00686   0.00245   0.0096   0.4595   0.9493
   2.250   0.2021   0.00761   0.00266   0.0120   0.3080   0.9533
   2.500   0.2188   0.00802   0.00276   0.0142   0.2267   0.9576
   2.750   0.2471   0.00840   0.00291   0.0139   0.1681   0.9588
   3.000   0.2759   0.00873   0.00307   0.0134   0.1244   0.9599
   3.250   0.3051   0.00906   0.00324   0.0128   0.0898   0.9611
   3.500   0.3342   0.00938   0.00343   0.0123   0.0605   0.9624
   3.750   0.3632   0.00968   0.00363   0.0119   0.0463   0.9639
   4.000   0.3919   0.00994   0.00388   0.0115   0.0415   0.9656
   4.250   0.4071   0.01008   0.00403   0.0143   0.0402   0.9709
   4.500   0.4392   0.01031   0.00427   0.0132   0.0383   0.9714
   4.750   0.4715   0.01059   0.00454   0.0120   0.0362   0.9719
   5.000   0.5027   0.01098   0.00496   0.0109   0.0343   0.9725
   5.250   0.5332   0.01143   0.00545   0.0101   0.0331   0.9731
   5.500   0.5647   0.01167   0.00571   0.0090   0.0324   0.9738
   5.750   0.5954   0.01195   0.00601   0.0082   0.0314   0.9746
   6.000   0.6251   0.01228   0.00637   0.0075   0.0304   0.9756
   6.250   0.6544   0.01260   0.00670   0.0069   0.0293   0.9768
   6.500   0.6823   0.01295   0.00705   0.0066   0.0281   0.9783
   6.750   0.7052   0.01371   0.00785   0.0072   0.0267   0.9804
   7.000   0.7240   0.01433   0.00854   0.0090   0.0259   0.9836
   7.250   0.7558   0.01448   0.00872   0.0078   0.0252   0.9841
   7.500   0.7868   0.01473   0.00900   0.0068   0.0242   0.9847
   7.750   0.8168   0.01504   0.00934   0.0059   0.0232   0.9853
   8.000   0.8468   0.01532   0.00964   0.0051   0.0222   0.9861
   8.250   0.8750   0.01586   0.01018   0.0045   0.0212   0.9870
   8.500   0.9012   0.01669   0.01112   0.0043   0.0202   0.9880
   8.750   0.9303   0.01684   0.01131   0.0037   0.0195   0.9891
   9.000   0.9579   0.01713   0.01165   0.0033   0.0186   0.9904
   9.250   0.9850   0.01739   0.01193   0.0031   0.0179   0.9918
   9.500   1.0112   0.01762   0.01218   0.0030   0.0172   0.9934
   9.750   1.0354   0.01836   0.01296   0.0032   0.0163   0.9945
  10.000   1.0618   0.01908   0.01379   0.0028   0.0157   0.9951
  10.250   1.0901   0.01939   0.01417   0.0023   0.0151   0.9959
  10.500   1.1181   0.01972   0.01455   0.0017   0.0144   0.9967
  10.750   1.1459   0.02003   0.01489   0.0011   0.0138   0.9977
  11.000   1.1730   0.02042   0.01531   0.0007   0.0133   0.9987
  11.250   1.1944   0.02154   0.01653   0.0011   0.0126   0.9997
  11.500   1.2072   0.02251   0.01764   0.0034   0.0122   1.0000
  11.750   1.2174   0.02306   0.01829   0.0064   0.0120   1.0000
  12.000   1.2261   0.02367   0.01900   0.0097   0.0117   1.0000
  12.250   1.2330   0.02431   0.01974   0.0133   0.0114   1.0000
  12.500   1.2386   0.02495   0.02048   0.0171   0.0112   1.0000
  12.750   1.2423   0.02554   0.02114   0.0213   0.0109   1.0000
  13.000   1.2401   0.02601   0.02168   0.0267   0.0107   1.0000
  13.250   1.2383   0.02658   0.02232   0.0318   0.0105   1.0000
  13.500   1.2396   0.02722   0.02303   0.0360   0.0103   1.0000
  13.750   1.2415   0.02803   0.02392   0.0399   0.0101   1.0000
  14.000   1.2410   0.02914   0.02511   0.0438   0.0099   1.0000
  14.250   1.2344   0.03084   0.02696   0.0480   0.0097   1.0000
  14.500   1.2156   0.03371   0.03008   0.0529   0.0094   1.0000
  14.750   1.2110   0.03573   0.03226   0.0556   0.0093   1.0000
  15.000   1.2093   0.03765   0.03432   0.0577   0.0092   1.0000
  15.250   1.2066   0.03979   0.03660   0.0594   0.0091   1.0000
  15.500   1.1984   0.04265   0.03962   0.0606   0.0091   1.0000
  15.750   1.1862   0.04624   0.04338   0.0611   0.0090   1.0000
  16.000   1.1673   0.05123   0.04856   0.0601   0.0090   1.0000
  16.250   1.1368   0.05930   0.05685   0.0558   0.0090   1.0000
  16.500   1.0187   0.09146   0.08943   0.0340   0.0096   1.0000
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