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NACA 1410 (naca1410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 1410 (naca1410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.32 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca1410-il-1000000-n5.txt
Download as CSV file: xf-naca1410-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 1410                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.0860   0.10096   0.09860  -0.0040   1.0000   0.0061
 -16.500  -1.2328   0.06971   0.06695  -0.0220   1.0000   0.0056
 -16.250  -1.2897   0.05406   0.05100  -0.0333   1.0000   0.0055
 -16.000  -1.3138   0.04558   0.04230  -0.0401   1.0000   0.0054
 -15.750  -1.3270   0.04003   0.03657  -0.0441   1.0000   0.0055
 -15.500  -1.3346   0.03621   0.03259  -0.0459   1.0000   0.0055
 -15.250  -1.3383   0.03344   0.02969  -0.0460   1.0000   0.0056
 -15.000  -1.3390   0.03135   0.02747  -0.0451   1.0000   0.0057
 -14.750  -1.3371   0.02970   0.02571  -0.0434   1.0000   0.0058
 -14.500  -1.3325   0.02833   0.02423  -0.0414   1.0000   0.0059
 -14.250  -1.3221   0.02708   0.02287  -0.0400   1.0000   0.0060
 -14.000  -1.3092   0.02593   0.02161  -0.0388   1.0000   0.0062
 -13.750  -1.2944   0.02487   0.02045  -0.0377   1.0000   0.0063
 -13.500  -1.2783   0.02388   0.01936  -0.0367   1.0000   0.0065
 -13.250  -1.2608   0.02296   0.01834  -0.0358   1.0000   0.0067
 -13.000  -1.2424   0.02212   0.01739  -0.0349   1.0000   0.0068
 -12.750  -1.2229   0.02134   0.01652  -0.0341   1.0000   0.0069
 -12.500  -1.2044   0.02039   0.01548  -0.0332   1.0000   0.0073
 -12.250  -1.1846   0.01957   0.01459  -0.0324   1.0000   0.0076
 -12.000  -1.1638   0.01886   0.01381  -0.0316   1.0000   0.0079
 -11.750  -1.1424   0.01820   0.01309  -0.0309   1.0000   0.0083
 -11.500  -1.1205   0.01760   0.01243  -0.0302   1.0000   0.0087
 -11.250  -1.0983   0.01705   0.01180  -0.0295   1.0000   0.0091
 -11.000  -1.0757   0.01654   0.01121  -0.0289   1.0000   0.0093
 -10.750  -1.0540   0.01591   0.01054  -0.0280   1.0000   0.0100
 -10.500  -1.0318   0.01538   0.00997  -0.0273   1.0000   0.0107
 -10.250  -1.0094   0.01491   0.00946  -0.0264   1.0000   0.0113
 -10.000  -0.9870   0.01447   0.00898  -0.0256   1.0000   0.0120
  -9.750  -0.9646   0.01407   0.00851  -0.0247   1.0000   0.0126
  -9.500  -0.9424   0.01364   0.00808  -0.0238   1.0000   0.0137
  -9.250  -0.9199   0.01328   0.00770  -0.0229   1.0000   0.0150
  -9.000  -0.8974   0.01295   0.00734  -0.0219   1.0000   0.0161
  -8.750  -0.8751   0.01261   0.00701  -0.0210   1.0000   0.0175
  -8.500  -0.8494   0.01232   0.00671  -0.0207   0.9995   0.0190
  -8.250  -0.8182   0.01203   0.00640  -0.0216   0.9981   0.0204
  -8.000  -0.7866   0.01178   0.00611  -0.0225   0.9966   0.0213
  -7.750  -0.7549   0.01143   0.00576  -0.0236   0.9951   0.0229
  -7.500  -0.7231   0.01115   0.00548  -0.0246   0.9934   0.0243
  -7.250  -0.6922   0.01089   0.00520  -0.0254   0.9910   0.0255
  -7.000  -0.6602   0.01066   0.00494  -0.0264   0.9886   0.0266
  -6.750  -0.6277   0.01045   0.00471  -0.0274   0.9863   0.0273
  -6.500  -0.5961   0.01019   0.00442  -0.0283   0.9834   0.0281
  -6.250  -0.5669   0.00986   0.00408  -0.0287   0.9784   0.0298
  -6.000  -0.5356   0.00960   0.00381  -0.0295   0.9744   0.0313
  -5.750  -0.5067   0.00937   0.00358  -0.0298   0.9683   0.0326
  -5.500  -0.4768   0.00917   0.00335  -0.0302   0.9622   0.0339
  -5.250  -0.4487   0.00898   0.00314  -0.0302   0.9543   0.0346
  -5.000  -0.4203   0.00881   0.00294  -0.0302   0.9459   0.0353
  -4.750  -0.3932   0.00860   0.00271  -0.0300   0.9354   0.0381
  -4.500  -0.3661   0.00842   0.00252  -0.0297   0.9244   0.0408
  -4.250  -0.3390   0.00827   0.00235  -0.0294   0.9125   0.0438
  -4.000  -0.3123   0.00809   0.00217  -0.0291   0.8994   0.0514
  -3.750  -0.2856   0.00791   0.00201  -0.0288   0.8853   0.0642
  -3.500  -0.2587   0.00775   0.00186  -0.0285   0.8705   0.0778
  -3.250  -0.2317   0.00762   0.00172  -0.0283   0.8547   0.0910
  -3.000  -0.2046   0.00749   0.00160  -0.0281   0.8382   0.1059
  -2.750  -0.1775   0.00736   0.00148  -0.0279   0.8211   0.1240
  -2.500  -0.1505   0.00722   0.00137  -0.0276   0.8027   0.1495
  -2.250  -0.1235   0.00709   0.00128  -0.0275   0.7844   0.1757
  -2.000  -0.0965   0.00697   0.00119  -0.0273   0.7648   0.2056
  -1.750  -0.0694   0.00685   0.00112  -0.0271   0.7444   0.2386
  -1.500  -0.0422   0.00677   0.00107  -0.0269   0.7217   0.2691
  -1.250  -0.0149   0.00675   0.00102  -0.0268   0.6971   0.2886
  -0.750   0.0388   0.00649   0.00091  -0.0265   0.6505   0.3769
  -0.500   0.0654   0.00630   0.00091  -0.0263   0.6286   0.4589
  -0.250   0.0928   0.00628   0.00091  -0.0262   0.6077   0.4926
   0.000   0.1204   0.00627   0.00091  -0.0261   0.5863   0.5180
   0.250   0.1479   0.00630   0.00092  -0.0260   0.5641   0.5371
   0.500   0.1753   0.00633   0.00093  -0.0259   0.5388   0.5590
   0.750   0.2026   0.00634   0.00096  -0.0258   0.5147   0.5860
   1.000   0.2296   0.00630   0.00099  -0.0256   0.4932   0.6309
   1.250   0.2563   0.00626   0.00104  -0.0253   0.4716   0.6815
   1.500   0.2824   0.00631   0.00110  -0.0250   0.4337   0.7278
   1.750   0.3079   0.00642   0.00118  -0.0245   0.3883   0.7732
   2.000   0.3337   0.00646   0.00127  -0.0240   0.3610   0.8159
   2.500   0.3847   0.00673   0.00149  -0.0229   0.2945   0.8807
   2.750   0.4098   0.00690   0.00161  -0.0222   0.2629   0.9086
   3.000   0.4356   0.00708   0.00175  -0.0217   0.2362   0.9351
   3.250   0.4628   0.00738   0.00191  -0.0216   0.1970   0.9537
   3.500   0.4922   0.00767   0.00207  -0.0220   0.1650   0.9665
   3.750   0.5228   0.00798   0.00225  -0.0227   0.1353   0.9767
   4.000   0.5539   0.00830   0.00244  -0.0235   0.1070   0.9852
   4.250   0.5863   0.00860   0.00263  -0.0247   0.0865   0.9909
   4.500   0.6176   0.00887   0.00283  -0.0255   0.0708   0.9952
   4.750   0.6497   0.00919   0.00306  -0.0266   0.0535   0.9982
   5.000   0.6785   0.00947   0.00327  -0.0270   0.0436   1.0000
   5.250   0.7030   0.00970   0.00348  -0.0263   0.0389   1.0000
   5.500   0.7278   0.00991   0.00369  -0.0257   0.0366   1.0000
   5.750   0.7527   0.01015   0.00391  -0.0251   0.0346   1.0000
   6.000   0.7777   0.01041   0.00417  -0.0246   0.0323   1.0000
   6.250   0.8030   0.01066   0.00444  -0.0241   0.0313   1.0000
   6.500   0.8285   0.01089   0.00468  -0.0236   0.0308   1.0000
   6.750   0.8541   0.01112   0.00493  -0.0232   0.0299   1.0000
   7.000   0.8796   0.01138   0.00520  -0.0228   0.0289   1.0000
   7.250   0.9050   0.01165   0.00549  -0.0224   0.0277   1.0000
   7.500   0.9301   0.01196   0.00581  -0.0220   0.0265   1.0000
   7.750   0.9548   0.01233   0.00619  -0.0215   0.0251   1.0000
   8.000   0.9798   0.01266   0.00654  -0.0211   0.0242   1.0000
   8.250   1.0053   0.01291   0.00683  -0.0208   0.0237   1.0000
   8.500   1.0306   0.01319   0.00714  -0.0204   0.0229   1.0000
   8.750   1.0557   0.01348   0.00746  -0.0200   0.0219   1.0000
   9.000   1.0805   0.01380   0.00777  -0.0196   0.0206   1.0000
   9.250   1.1049   0.01417   0.00814  -0.0192   0.0193   1.0000
   9.500   1.1291   0.01454   0.00856  -0.0187   0.0184   1.0000
   9.750   1.1535   0.01488   0.00893  -0.0182   0.0174   1.0000
  10.000   1.1775   0.01524   0.00931  -0.0178   0.0161   1.0000
  10.250   1.2009   0.01566   0.00971  -0.0172   0.0145   1.0000
  10.500   1.2240   0.01610   0.01019  -0.0166   0.0134   1.0000
  10.750   1.2467   0.01657   0.01068  -0.0160   0.0123   1.0000
  11.000   1.2688   0.01709   0.01123  -0.0153   0.0113   1.0000
  11.250   1.2903   0.01764   0.01182  -0.0145   0.0105   1.0000
  11.500   1.3118   0.01818   0.01241  -0.0137   0.0099   1.0000
  11.750   1.3324   0.01877   0.01305  -0.0128   0.0094   1.0000
  12.000   1.3523   0.01940   0.01373  -0.0119   0.0088   1.0000
  12.250   1.3711   0.02011   0.01448  -0.0108   0.0083   1.0000
  12.500   1.3890   0.02085   0.01530  -0.0096   0.0078   1.0000
  12.750   1.4071   0.02152   0.01604  -0.0085   0.0076   1.0000
  13.000   1.4241   0.02224   0.01683  -0.0072   0.0073   1.0000
  13.250   1.4395   0.02301   0.01768  -0.0058   0.0070   1.0000
  13.500   1.4517   0.02383   0.01857  -0.0038   0.0067   1.0000
  13.750   1.4621   0.02474   0.01955  -0.0017   0.0065   1.0000
  14.000   1.4713   0.02576   0.02065   0.0003   0.0063   1.0000
  14.250   1.4787   0.02695   0.02193   0.0023   0.0060   1.0000
  14.500   1.4842   0.02834   0.02341   0.0042   0.0058   1.0000
  14.750   1.4893   0.02983   0.02500   0.0058   0.0057   1.0000
  15.000   1.4949   0.03138   0.02665   0.0071   0.0056   1.0000
  15.250   1.4991   0.03316   0.02854   0.0081   0.0055   1.0000
  15.500   1.5018   0.03521   0.03070   0.0089   0.0054   1.0000
  15.750   1.5030   0.03757   0.03318   0.0092   0.0054   1.0000
  16.000   1.5023   0.04031   0.03604   0.0092   0.0053   1.0000
  16.250   1.4999   0.04347   0.03932   0.0087   0.0052   1.0000
  16.500   1.4951   0.04712   0.04311   0.0076   0.0051   1.0000
  16.750   1.4877   0.05138   0.04750   0.0061   0.0051   1.0000
  17.000   1.4772   0.05629   0.05255   0.0040   0.0050   1.0000
  17.250   1.4630   0.06198   0.05838   0.0013   0.0050   1.0000
  17.500   1.4444   0.06857   0.06513  -0.0020   0.0050   1.0000
  17.750   1.4203   0.07629   0.07300  -0.0059   0.0050   1.0000
  18.000   1.3905   0.08528   0.08217  -0.0106   0.0050   1.0000
  18.250   1.3541   0.09577   0.09283  -0.0161   0.0050   1.0000
  18.500   1.3107   0.10791   0.10516  -0.0224   0.0051   1.0000
  18.750   1.2597   0.12204   0.11947  -0.0298   0.0052   1.0000
  19.000   1.2059   0.13730   0.13492  -0.0380   0.0053   1.0000
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