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EPPLER 715 AIRFOIL (e715-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 715 AIRFOIL (e715-il)
Reynolds number: 100,000
Max Cl/Cd: 44.25 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e715-il-100000-n5.txt
Download as CSV file: xf-e715-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5587   0.10045   0.09580  -0.0200   1.0000   0.0202
 -12.500  -0.5866   0.08930   0.08460  -0.0270   1.0000   0.0199
 -12.250  -0.6087   0.08052   0.07575  -0.0330   1.0000   0.0195
 -12.000  -0.6313   0.07249   0.06758  -0.0389   1.0000   0.0192
 -11.750  -0.6521   0.06554   0.06048  -0.0441   1.0000   0.0191
 -11.500  -0.6682   0.05978   0.05455  -0.0483   1.0000   0.0190
 -11.250  -0.6821   0.05460   0.04920  -0.0520   1.0000   0.0191
 -11.000  -0.6909   0.04996   0.04428  -0.0560   0.9029   0.0193
 -10.750  -0.6964   0.04613   0.03994  -0.0587   0.8393   0.0197
 -10.500  -0.7020   0.04343   0.03684  -0.0584   0.8094   0.0200
 -10.250  -0.7040   0.04130   0.03442  -0.0573   0.7895   0.0208
 -10.000  -0.6972   0.03973   0.03270  -0.0566   0.7738   0.0216
  -9.750  -0.6881   0.03803   0.03075  -0.0559   0.7611   0.0227
  -9.500  -0.6766   0.03619   0.02862  -0.0552   0.7508   0.0239
  -9.250  -0.6627   0.03428   0.02633  -0.0543   0.7415   0.0253
  -9.000  -0.6476   0.03263   0.02461  -0.0536   0.7328   0.0264
  -8.750  -0.6313   0.03132   0.02317  -0.0529   0.7250   0.0283
  -8.500  -0.6127   0.03005   0.02164  -0.0523   0.7172   0.0314
  -8.250  -0.5956   0.02877   0.02030  -0.0516   0.7105   0.0339
  -8.000  -0.5764   0.02761   0.01898  -0.0510   0.7042   0.0378
  -7.750  -0.5575   0.02647   0.01779  -0.0504   0.6981   0.0424
  -7.500  -0.5374   0.02548   0.01662  -0.0496   0.6932   0.0483
  -7.250  -0.5171   0.02448   0.01559  -0.0492   0.6877   0.0558
  -7.000  -0.4963   0.02351   0.01458  -0.0486   0.6825   0.0655
  -6.750  -0.4750   0.02263   0.01363  -0.0480   0.6781   0.0785
  -6.500  -0.4525   0.02181   0.01279  -0.0477   0.6732   0.0963
  -6.250  -0.4300   0.02097   0.01203  -0.0474   0.6684   0.1205
  -6.000  -0.4070   0.02023   0.01134  -0.0471   0.6644   0.1523
  -5.750  -0.3840   0.01952   0.01070  -0.0468   0.6611   0.1902
  -5.500  -0.3599   0.01890   0.01022  -0.0467   0.6568   0.2344
  -5.250  -0.3358   0.01841   0.00987  -0.0464   0.6527   0.2828
  -5.000  -0.3111   0.01813   0.00971  -0.0460   0.6491   0.3312
  -4.750  -0.2855   0.01811   0.00970  -0.0454   0.6460   0.3720
  -4.500  -0.2585   0.01822   0.00978  -0.0451   0.6419   0.4035
  -4.250  -0.2312   0.01837   0.00983  -0.0449   0.6383   0.4280
  -4.000  -0.2039   0.01854   0.00985  -0.0446   0.6351   0.4478
  -3.750  -0.1766   0.01868   0.00983  -0.0443   0.6323   0.4647
  -3.500  -0.1493   0.01882   0.00981  -0.0440   0.6294   0.4789
  -3.250  -0.1218   0.01892   0.00983  -0.0439   0.6256   0.4915
  -3.000  -0.0943   0.01899   0.00976  -0.0439   0.6222   0.5033
  -2.750  -0.0669   0.01905   0.00972  -0.0437   0.6193   0.5137
  -2.500  -0.0395   0.01909   0.00966  -0.0435   0.6169   0.5229
  -2.250  -0.0119   0.01913   0.00952  -0.0434   0.6146   0.5330
  -2.000   0.0155   0.01918   0.00959  -0.0434   0.6110   0.5407
  -1.750   0.0432   0.01922   0.00954  -0.0435   0.6076   0.5491
  -1.500   0.0706   0.01924   0.00953  -0.0434   0.6047   0.5559
  -1.250   0.0984   0.01927   0.00945  -0.0434   0.6023   0.5638
  -1.000   0.1260   0.01928   0.00941  -0.0433   0.6002   0.5700
  -0.750   0.1537   0.01935   0.00942  -0.0434   0.5974   0.5774
  -0.500   0.1810   0.01943   0.00955  -0.0435   0.5939   0.5831
  -0.250   0.2085   0.01951   0.00961  -0.0436   0.5908   0.5893
   0.000   0.2363   0.01959   0.00965  -0.0437   0.5883   0.5954
   0.250   0.2640   0.01963   0.00968  -0.0437   0.5860   0.6008
   0.500   0.2921   0.01969   0.00966  -0.0438   0.5839   0.6068
   0.750   0.3192   0.01988   0.00991  -0.0440   0.5804   0.6123
   1.000   0.3462   0.02006   0.01016  -0.0442   0.5771   0.6179
   1.250   0.3738   0.02023   0.01033  -0.0443   0.5742   0.6242
   1.500   0.4011   0.02032   0.01045  -0.0443   0.5716   0.6297
   1.750   0.4289   0.02040   0.01052  -0.0443   0.5694   0.6360
   2.000   0.4564   0.02057   0.01072  -0.0444   0.5669   0.6425
   2.250   0.4822   0.02092   0.01121  -0.0445   0.5629   0.6491
   2.500   0.5091   0.02117   0.01152  -0.0447   0.5594   0.6568
   2.750   0.5366   0.02130   0.01172  -0.0447   0.5566   0.6642
   3.000   0.5645   0.02141   0.01187  -0.0448   0.5543   0.6734
   3.250   0.5921   0.02153   0.01206  -0.0447   0.5519   0.6835
   3.500   0.6157   0.02203   0.01279  -0.0448   0.5468   0.6951
   3.750   0.6415   0.02225   0.01316  -0.0447   0.5431   0.7098
   4.000   0.6683   0.02229   0.01333  -0.0444   0.5401   0.7305
   4.250   0.6956   0.02219   0.01342  -0.0440   0.5378   0.7637
   4.500   0.7247   0.02250   0.01420  -0.0449   0.5322   0.8531
   4.750   0.7639   0.02277   0.01461  -0.0476   0.5274   1.0000
   5.000   0.7916   0.02288   0.01470  -0.0476   0.5242   1.0000
   5.250   0.8194   0.02297   0.01477  -0.0475   0.5211   1.0000
   5.500   0.8390   0.02377   0.01573  -0.0471   0.5139   1.0000
   5.750   0.8659   0.02383   0.01582  -0.0469   0.5097   1.0000
   6.000   0.8956   0.02364   0.01562  -0.0467   0.5067   1.0000
   6.250   0.9129   0.02450   0.01667  -0.0460   0.4982   1.0000
   6.500   0.9409   0.02435   0.01655  -0.0457   0.4937   1.0000
   6.750   0.9627   0.02472   0.01705  -0.0451   0.4869   1.0000
   7.000   0.9871   0.02480   0.01722  -0.0446   0.4803   1.0000
   7.250   1.0132   0.02470   0.01719  -0.0441   0.4744   1.0000
   7.500   1.0336   0.02501   0.01766  -0.0433   0.4658   1.0000
   7.750   1.0566   0.02506   0.01782  -0.0425   0.4578   1.0000
   8.000   1.0806   0.02494   0.01780  -0.0418   0.4490   1.0000
   8.250   1.0975   0.02536   0.01838  -0.0406   0.4378   1.0000
   8.500   1.1166   0.02555   0.01871  -0.0395   0.4264   1.0000
   8.750   1.1354   0.02571   0.01898  -0.0384   0.4138   1.0000
   9.000   1.1515   0.02602   0.01940  -0.0370   0.3993   1.0000
   9.250   1.1647   0.02647   0.01992  -0.0354   0.3826   1.0000
   9.500   1.1763   0.02696   0.02042  -0.0336   0.3639   1.0000
   9.750   1.1824   0.02763   0.02107  -0.0312   0.3440   1.0000
  10.000   1.1814   0.02904   0.02242  -0.0290   0.3230   1.0000
  10.250   1.1814   0.03063   0.02388  -0.0274   0.3009   1.0000
  10.500   1.1785   0.03274   0.02592  -0.0261   0.2796   1.0000
  10.750   1.1754   0.03500   0.02805  -0.0250   0.2590   1.0000
  11.000   1.1716   0.03745   0.03042  -0.0240   0.2395   1.0000
  11.250   1.1682   0.03996   0.03287  -0.0232   0.2213   1.0000
  11.500   1.1647   0.04256   0.03539  -0.0226   0.2040   1.0000
  11.750   1.1619   0.04516   0.03793  -0.0220   0.1883   1.0000
  12.000   1.1591   0.04783   0.04055  -0.0216   0.1733   1.0000
  12.250   1.1568   0.05052   0.04323  -0.0212   0.1594   1.0000
  12.500   1.1550   0.05323   0.04592  -0.0210   0.1464   1.0000
  12.750   1.1536   0.05596   0.04864  -0.0208   0.1344   1.0000
  13.000   1.1525   0.05880   0.05146  -0.0208   0.1233   1.0000
  13.250   1.1511   0.06175   0.05439  -0.0209   0.1133   1.0000
  13.500   1.1501   0.06477   0.05741  -0.0212   0.1038   1.0000
  13.750   1.1507   0.06769   0.06037  -0.0214   0.0952   1.0000
  14.000   1.1492   0.07091   0.06357  -0.0218   0.0881   1.0000
  14.250   1.1496   0.07401   0.06675  -0.0222   0.0808   1.0000
  14.500   1.1488   0.07729   0.07003  -0.0228   0.0749   1.0000
  14.750   1.1490   0.08055   0.07340  -0.0234   0.0691   1.0000
  15.000   1.1473   0.08408   0.07692  -0.0241   0.0645   1.0000
  15.250   1.1479   0.08742   0.08039  -0.0249   0.0594   1.0000
  15.500   1.1462   0.09110   0.08409  -0.0258   0.0559   1.0000
  15.750   1.1467   0.09451   0.08759  -0.0266   0.0521   1.0000
  16.000   1.1460   0.09823   0.09142  -0.0277   0.0485   1.0000
  16.250   1.1440   0.10213   0.09534  -0.0290   0.0459   1.0000
  16.500   1.1442   0.10576   0.09908  -0.0300   0.0431   1.0000
  16.750   1.1434   0.10966   0.10311  -0.0314   0.0404   1.0000
  17.000   1.1414   0.11380   0.10732  -0.0330   0.0383   1.0000
  17.250   1.1402   0.11767   0.11119  -0.0345   0.0363   1.0000
  17.500   1.1389   0.12191   0.11565  -0.0362   0.0344   1.0000
  17.750   1.1364   0.12637   0.12025  -0.0382   0.0326   1.0000
  18.000   1.1338   0.13086   0.12484  -0.0403   0.0310   1.0000
  18.250   1.1323   0.13505   0.12904  -0.0424   0.0297   1.0000
  18.500   1.1283   0.14002   0.13418  -0.0449   0.0284   1.0000
  18.750   1.1225   0.14556   0.13992  -0.0478   0.0273   1.0000
  19.000   1.1160   0.15137   0.14591  -0.0511   0.0263   1.0000
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