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EPPLER 715 AIRFOIL (e715-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 715 AIRFOIL (e715-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.36 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e715-il-1000000-n5.txt
Download as CSV file: xf-e715-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 715 AIRFOIL                              
  
 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  -0.8912   0.10000   0.09735  -0.0143   1.0000   0.0025
 -16.500  -0.9157   0.09112   0.08834  -0.0194   1.0000   0.0024
 -16.250  -0.9489   0.08093   0.07799  -0.0255   1.0000   0.0025
 -16.000  -0.9592   0.07514   0.07209  -0.0289   1.0000   0.0024
 -15.500  -0.9828   0.06132   0.05757  -0.0403   0.8102   0.0024
 -15.250  -1.0067   0.05509   0.05108  -0.0436   0.7745   0.0024
 -15.000  -1.0152   0.05112   0.04693  -0.0454   0.7466   0.0024
 -14.750  -1.0335   0.04612   0.04175  -0.0477   0.7280   0.0025
 -14.500  -1.0424   0.04241   0.03789  -0.0492   0.7115   0.0026
 -14.250  -1.0472   0.03924   0.03458  -0.0503   0.6972   0.0025
 -14.000  -1.0554   0.03574   0.03095  -0.0516   0.6852   0.0025
 -13.750  -1.0573   0.03290   0.02799  -0.0526   0.6739   0.0026
 -13.500  -1.0606   0.02993   0.02488  -0.0539   0.6636   0.0025
 -13.250  -1.0643   0.02743   0.02225  -0.0545   0.6547   0.0026
 -12.750  -1.0636   0.02474   0.01933  -0.0507   0.6380   0.0027
 -12.250  -1.0382   0.02273   0.01710  -0.0486   0.6235   0.0027
 -12.000  -1.0215   0.02188   0.01615  -0.0478   0.6167   0.0028
 -11.750  -1.0035   0.02107   0.01524  -0.0470   0.6114   0.0028
 -11.500  -0.9842   0.02032   0.01440  -0.0463   0.6060   0.0029
 -11.250  -0.9638   0.01962   0.01362  -0.0457   0.6008   0.0031
 -11.000  -0.9426   0.01895   0.01286  -0.0452   0.5965   0.0031
 -10.750  -0.9206   0.01832   0.01215  -0.0447   0.5922   0.0032
 -10.500  -0.8977   0.01775   0.01150  -0.0443   0.5877   0.0033
 -10.000  -0.8506   0.01669   0.01028  -0.0435   0.5799   0.0035
  -9.750  -0.8263   0.01620   0.00972  -0.0431   0.5759   0.0036
  -9.500  -0.8024   0.01564   0.00909  -0.0428   0.5722   0.0039
  -9.250  -0.7777   0.01516   0.00855  -0.0425   0.5689   0.0041
  -9.000  -0.7524   0.01474   0.00807  -0.0422   0.5662   0.0043
  -8.750  -0.7268   0.01433   0.00762  -0.0420   0.5635   0.0046
  -8.500  -0.7008   0.01396   0.00719  -0.0418   0.5606   0.0049
  -8.250  -0.6746   0.01362   0.00679  -0.0416   0.5578   0.0053
  -8.000  -0.6485   0.01325   0.00638  -0.0414   0.5550   0.0060
  -7.750  -0.6220   0.01292   0.00601  -0.0413   0.5523   0.0068
  -7.500  -0.5952   0.01261   0.00567  -0.0411   0.5501   0.0077
  -7.250  -0.5683   0.01230   0.00534  -0.0410   0.5476   0.0091
  -7.000  -0.5413   0.01201   0.00503  -0.0409   0.5452   0.0107
  -6.500  -0.4868   0.01147   0.00445  -0.0408   0.5407   0.0156
  -6.250  -0.4596   0.01121   0.00418  -0.0407   0.5385   0.0197
  -6.000  -0.4321   0.01095   0.00392  -0.0407   0.5366   0.0248
  -5.750  -0.4045   0.01069   0.00368  -0.0407   0.5348   0.0306
  -5.250  -0.3496   0.01011   0.00319  -0.0406   0.5306   0.0535
  -5.000  -0.3220   0.00985   0.00297  -0.0406   0.5286   0.0687
  -4.750  -0.2942   0.00960   0.00277  -0.0406   0.5268   0.0851
  -4.500  -0.2665   0.00935   0.00258  -0.0407   0.5249   0.1044
  -4.250  -0.2387   0.00911   0.00240  -0.0407   0.5230   0.1274
  -4.000  -0.2110   0.00884   0.00222  -0.0407   0.5212   0.1574
  -3.750  -0.1829   0.00859   0.00207  -0.0408   0.5196   0.1847
  -3.500  -0.1547   0.00838   0.00193  -0.0409   0.5179   0.2110
  -3.250  -0.1267   0.00814   0.00180  -0.0409   0.5162   0.2439
  -3.000  -0.0987   0.00788   0.00166  -0.0410   0.5145   0.2830
  -2.750  -0.0705   0.00768   0.00156  -0.0411   0.5127   0.3183
  -2.500  -0.0422   0.00751   0.00148  -0.0412   0.5109   0.3504
  -2.250  -0.0137   0.00741   0.00143  -0.0413   0.5090   0.3750
  -2.000   0.0151   0.00736   0.00140  -0.0414   0.5070   0.3959
  -1.750   0.0440   0.00731   0.00138  -0.0415   0.5057   0.4115
  -1.500   0.0732   0.00728   0.00137  -0.0417   0.5043   0.4241
  -1.250   0.1023   0.00726   0.00137  -0.0418   0.5027   0.4341
  -1.000   0.1316   0.00726   0.00136  -0.0420   0.5009   0.4415
  -0.750   0.1607   0.00726   0.00137  -0.0421   0.4990   0.4484
  -0.500   0.1900   0.00727   0.00136  -0.0423   0.4972   0.4540
  -0.250   0.2191   0.00728   0.00137  -0.0425   0.4955   0.4597
   0.000   0.2482   0.00730   0.00138  -0.0426   0.4937   0.4653
   0.250   0.2773   0.00735   0.00140  -0.0428   0.4917   0.4695
   0.500   0.3065   0.00735   0.00141  -0.0430   0.4902   0.4731
   0.750   0.3356   0.00735   0.00144  -0.0431   0.4887   0.4767
   1.000   0.3648   0.00737   0.00146  -0.0433   0.4869   0.4809
   1.250   0.3940   0.00739   0.00149  -0.0435   0.4849   0.4846
   1.500   0.4231   0.00741   0.00151  -0.0437   0.4828   0.4878
   1.750   0.4521   0.00743   0.00154  -0.0439   0.4807   0.4908
   2.000   0.4810   0.00746   0.00158  -0.0440   0.4784   0.4937
   2.250   0.5100   0.00750   0.00162  -0.0442   0.4761   0.4963
   2.500   0.5391   0.00752   0.00166  -0.0444   0.4736   0.4988
   2.750   0.5682   0.00755   0.00170  -0.0446   0.4705   0.5010
   3.000   0.5971   0.00757   0.00174  -0.0448   0.4670   0.5035
   3.250   0.6258   0.00760   0.00178  -0.0449   0.4634   0.5060
   3.500   0.6546   0.00764   0.00185  -0.0451   0.4601   0.5088
   3.750   0.6836   0.00767   0.00190  -0.0453   0.4561   0.5113
   4.000   0.7123   0.00771   0.00196  -0.0455   0.4514   0.5137
   4.250   0.7408   0.00778   0.00203  -0.0456   0.4467   0.5161
   4.500   0.7696   0.00781   0.00210  -0.0458   0.4417   0.5187
   4.750   0.7980   0.00787   0.00218  -0.0459   0.4356   0.5214
   5.000   0.8264   0.00794   0.00227  -0.0461   0.4297   0.5242
   5.250   0.8547   0.00802   0.00237  -0.0462   0.4214   0.5273
   5.500   0.8828   0.00812   0.00248  -0.0463   0.4115   0.5303
   5.750   0.9104   0.00826   0.00260  -0.0464   0.3996   0.5332
   6.000   0.9377   0.00843   0.00276  -0.0464   0.3854   0.5365
   6.250   0.9644   0.00866   0.00295  -0.0463   0.3663   0.5400
   6.500   0.9901   0.00898   0.00320  -0.0462   0.3430   0.5437
   6.750   1.0147   0.00943   0.00353  -0.0459   0.3131   0.5476
   7.000   1.0381   0.00995   0.00393  -0.0455   0.2796   0.5523
   7.250   1.0617   0.01044   0.00433  -0.0451   0.2533   0.5574
   7.500   1.0840   0.01101   0.00478  -0.0446   0.2233   0.5624
   7.750   1.1061   0.01156   0.00524  -0.0441   0.1976   0.5685
   8.000   1.1282   0.01208   0.00568  -0.0435   0.1752   0.5758
   8.250   1.1491   0.01264   0.00618  -0.0428   0.1537   0.5854
   8.500   1.1691   0.01320   0.00669  -0.0420   0.1330   0.5983
   8.750   1.1879   0.01379   0.00724  -0.0410   0.1146   0.6170
   9.000   1.2066   0.01430   0.00777  -0.0400   0.1005   0.6483
   9.250   1.2209   0.01452   0.00835  -0.0381   0.0886   0.7994
   9.500   1.2494   0.01492   0.00904  -0.0393   0.0753   1.0000
   9.750   1.2644   0.01561   0.00968  -0.0379   0.0656   1.0000
  10.000   1.2776   0.01631   0.01036  -0.0362   0.0572   1.0000
  10.250   1.2860   0.01699   0.01104  -0.0336   0.0516   1.0000
  10.750   1.2916   0.01923   0.01329  -0.0288   0.0403   1.0000
  11.000   1.2960   0.02074   0.01481  -0.0276   0.0357   1.0000
  11.250   1.3026   0.02228   0.01637  -0.0267   0.0319   1.0000
  11.500   1.3088   0.02394   0.01805  -0.0260   0.0286   1.0000
  11.750   1.3156   0.02560   0.01973  -0.0254   0.0258   1.0000
  12.000   1.3202   0.02747   0.02161  -0.0248   0.0225   1.0000
  12.250   1.3259   0.02927   0.02343  -0.0242   0.0202   1.0000
  12.500   1.3306   0.03116   0.02534  -0.0237   0.0182   1.0000
  12.750   1.3355   0.03304   0.02726  -0.0231   0.0161   1.0000
  13.000   1.3405   0.03494   0.02919  -0.0227   0.0151   1.0000
  13.250   1.3451   0.03687   0.03116  -0.0222   0.0139   1.0000
  13.500   1.3489   0.03888   0.03320  -0.0218   0.0124   1.0000
  13.750   1.3532   0.04089   0.03525  -0.0214   0.0117   1.0000
  14.000   1.3556   0.04308   0.03747  -0.0211   0.0102   1.0000
  14.250   1.3597   0.04517   0.03961  -0.0208   0.0095   1.0000
  14.500   1.3625   0.04748   0.04195  -0.0207   0.0087   1.0000
  14.750   1.3672   0.04963   0.04415  -0.0206   0.0080   1.0000
  15.000   1.3713   0.05192   0.04650  -0.0206   0.0075   1.0000
  15.250   1.3749   0.05427   0.04890  -0.0206   0.0070   1.0000
  15.500   1.3770   0.05685   0.05152  -0.0207   0.0063   1.0000
  15.750   1.3808   0.05927   0.05400  -0.0209   0.0059   1.0000
  16.000   1.3842   0.06179   0.05657  -0.0211   0.0057   1.0000
  16.250   1.3859   0.06454   0.05937  -0.0214   0.0050   1.0000
  16.500   1.3872   0.06740   0.06228  -0.0218   0.0046   1.0000
  16.750   1.3890   0.07026   0.06521  -0.0223   0.0043   1.0000
  17.000   1.3910   0.07311   0.06812  -0.0228   0.0041   1.0000
  17.250   1.3911   0.07627   0.07134  -0.0235   0.0038   1.0000
  17.500   1.3921   0.07935   0.07449  -0.0242   0.0036   1.0000
  17.750   1.3917   0.08272   0.07793  -0.0250   0.0035   1.0000
  18.000   1.3904   0.08623   0.08150  -0.0260   0.0033   1.0000
  18.250   1.3889   0.08984   0.08519  -0.0270   0.0031   1.0000
  18.500   1.3871   0.09358   0.08901  -0.0282   0.0030   1.0000
  18.750   1.3860   0.09725   0.09276  -0.0294   0.0028   1.0000
  19.000   1.3827   0.10134   0.09692  -0.0309   0.0026   1.0000
  19.250   1.3790   0.10553   0.10120  -0.0325   0.0025   1.0000
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