File: e387_11.100

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       XFOIL         Version 6.90
  
 Calculated polar for: Eppler 387                                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =  11.000
  
  alpha     CL        CD       CDp       CM    Top Xtr Bot Xtr
 ------- -------- --------- --------- -------- ------- -------
  -3.000   0.0560   0.02350   0.01498  -0.0988  0.9417  0.0994
  -2.900   0.0725   0.02284   0.01431  -0.0997  0.9384  0.1034
  -2.800   0.0920   0.02213   0.01360  -0.1013  0.9361  0.1128
  -2.700   0.1121   0.02138   0.01290  -0.1029  0.9341  0.1252
  -2.600   0.1330   0.02070   0.01217  -0.1045  0.9324  0.1443
  -2.400   0.1588   0.01962   0.01143  -0.1054  0.9245  0.1926
  -2.100   0.1963   0.01636   0.01058  -0.1056  0.9170  0.6517
  -1.900   0.2190   0.01570   0.01026  -0.1033  0.9104  1.0000
  -1.800   0.2368   0.01571   0.01006  -0.1045  0.9079  1.0000
  -1.700   0.2458   0.01589   0.01010  -0.1043  0.9028  1.0000
  -1.600   0.2595   0.01597   0.01003  -0.1048  0.8992  1.0000
  -1.500   0.2750   0.01599   0.00990  -0.1055  0.8965  1.0000
  -1.400   0.2863   0.01613   0.00992  -0.1057  0.8925  1.0000
  -1.300   0.2970   0.01627   0.00996  -0.1057  0.8882  1.0000
  -1.200   0.3107   0.01633   0.00990  -0.1061  0.8852  1.0000
  -1.100   0.3251   0.01635   0.00982  -0.1065  0.8829  1.0000
  -1.000   0.3331   0.01660   0.01000  -0.1063  0.8778  1.0000
  -0.900   0.3449   0.01670   0.01001  -0.1064  0.8743  1.0000
  -0.800   0.3581   0.01675   0.00997  -0.1066  0.8717  1.0000
  -0.700   0.3688   0.01690   0.01005  -0.1066  0.8682  1.0000
  -0.600   0.3785   0.01710   0.01017  -0.1066  0.8639  1.0000
  -0.500   0.3905   0.01718   0.01018  -0.1066  0.8609  1.0000
  -0.400   0.4031   0.01722   0.01015  -0.1066  0.8586  1.0000
  -0.300   0.4123   0.01748   0.01035  -0.1066  0.8543  1.0000
  -0.200   0.4227   0.01764   0.01047  -0.1066  0.8507  1.0000
  -0.100   0.4345   0.01772   0.01048  -0.1065  0.8479  1.0000
   0.000   0.4466   0.01777   0.01047  -0.1064  0.8458  1.0000
   0.100   0.4554   0.01808   0.01075  -0.1065  0.8412  1.0000
   0.200   0.4660   0.01824   0.01086  -0.1064  0.8378  1.0000
   0.300   0.4775   0.01832   0.01089  -0.1063  0.8353  1.0000
   0.400   0.4894   0.01837   0.01089  -0.1062  0.8333  1.0000
   0.500   0.4982   0.01873   0.01123  -0.1063  0.8286  1.0000
   0.600   0.5087   0.01890   0.01136  -0.1063  0.8254  1.0000
   0.700   0.5201   0.01898   0.01140  -0.1061  0.8229  1.0000
   0.800   0.5316   0.01903   0.01141  -0.1059  0.8209  1.0000
   0.900   0.5406   0.01942   0.01179  -0.1061  0.8164  1.0000
   1.000   0.5510   0.01961   0.01196  -0.1061  0.8132  1.0000
   1.100   0.5622   0.01970   0.01202  -0.1059  0.8107  1.0000
   1.200   0.5736   0.01976   0.01204  -0.1056  0.8087  1.0000
   1.300   0.5828   0.02015   0.01243  -0.1059  0.8045  1.0000
   1.400   0.5930   0.02037   0.01264  -0.1059  0.8011  1.0000
   1.500   0.6041   0.02048   0.01273  -0.1057  0.7986  1.0000
   1.600   0.6154   0.02054   0.01276  -0.1054  0.7966  1.0000
   1.700   0.6248   0.02092   0.01314  -0.1056  0.7928  1.0000
   1.800   0.6348   0.02119   0.01341  -0.1057  0.7893  1.0000
   1.900   0.6457   0.02131   0.01354  -0.1055  0.7867  1.0000
   2.000   0.6570   0.02137   0.01357  -0.1052  0.7846  1.0000
   2.100   0.6667   0.02171   0.01391  -0.1053  0.7812  1.0000
   2.200   0.6763   0.02204   0.01426  -0.1054  0.7774  1.0000
   2.300   0.6871   0.02218   0.01439  -0.1052  0.7746  1.0000
   2.400   0.6983   0.02223   0.01443  -0.1049  0.7725  1.0000
   2.500   0.7083   0.02250   0.01471  -0.1049  0.7695  1.0000
   2.600   0.7175   0.02292   0.01515  -0.1051  0.7653  1.0000
   2.700   0.7282   0.02305   0.01529  -0.1049  0.7625  1.0000
   2.800   0.7394   0.02309   0.01531  -0.1045  0.7603  1.0000
   2.900   0.7494   0.02335   0.01562  -0.1044  0.7572  1.0000
   3.000   0.7584   0.02378   0.01609  -0.1046  0.7528  1.0000
   3.100   0.7691   0.02389   0.01620  -0.1043  0.7499  1.0000
   3.200   0.7804   0.02389   0.01619  -0.1038  0.7476  1.0000
   3.300   0.7896   0.02428   0.01661  -0.1039  0.7437  1.0000
   3.400   0.7990   0.02461   0.01697  -0.1039  0.7396  1.0000
   3.500   0.8099   0.02464   0.01701  -0.1034  0.7368  1.0000
   3.600   0.8213   0.02456   0.01692  -0.1028  0.7346  1.0000
   3.700   0.8292   0.02516   0.01758  -0.1031  0.7292  1.0000
   3.800   0.8396   0.02523   0.01767  -0.1027  0.7255  1.0000
   3.900   0.8510   0.02505   0.01752  -0.1019  0.7228  1.0000
   4.000   0.8591   0.02546   0.01799  -0.1018  0.7172  1.0000
   4.100   0.8695   0.02542   0.01796  -0.1012  0.7129  1.0000
   4.200   0.8810   0.02512   0.01764  -0.1002  0.7100  1.0000
   4.300   0.8887   0.02559   0.01818  -0.1002  0.7036  1.0000
   4.400   0.8995   0.02546   0.01806  -0.0994  0.6998  1.0000
   4.500   0.9112   0.02517   0.01775  -0.0985  0.6972  1.0000
   4.600   0.9187   0.02575   0.01842  -0.0987  0.6906  1.0000
   4.700   0.9296   0.02564   0.01834  -0.0980  0.6871  1.0000
   4.800   0.9414   0.02542   0.01811  -0.0973  0.6848  1.0000
   5.000   0.9598   0.02594   0.01875  -0.0969  0.6748  1.0000
   5.100   0.9717   0.02568   0.01853  -0.0961  0.6724  1.0000
   5.300   0.9903   0.02610   0.01908  -0.0955  0.6620  1.0000
   5.400   0.9998   0.02619   0.01923  -0.0950  0.6569  1.0000
   5.500   1.0096   0.02612   0.01921  -0.0943  0.6511  1.0000
   5.600   1.0221   0.02551   0.01855  -0.0931  0.6476  1.0000
   5.700   1.0295   0.02575   0.01891  -0.0927  0.6392  1.0000
   5.800   1.0413   0.02518   0.01830  -0.0915  0.6343  1.0000
   5.900   1.0499   0.02511   0.01832  -0.0908  0.6261  1.0000
   6.000   1.0598   0.02484   0.01808  -0.0899  0.6194  1.0000
   6.100   1.0705   0.02445   0.01769  -0.0890  0.6128  1.0000
   6.200   1.0796   0.02434   0.01765  -0.0883  0.6050  1.0000
   6.300   1.0913   0.02379   0.01712  -0.0873  0.5992  1.0000
   6.400   1.0999   0.02374   0.01718  -0.0866  0.5905  1.0000
   6.500   1.1110   0.02333   0.01676  -0.0858  0.5843  1.0000
   6.600   1.1205   0.02315   0.01665  -0.0851  0.5761  1.0000
   6.700   1.1298   0.02301   0.01659  -0.0844  0.5678  1.0000
   6.800   1.1417   0.02253   0.01609  -0.0836  0.5615  1.0000
   6.900   1.1502   0.02244   0.01612  -0.0829  0.5516  1.0000
   7.000   1.1595   0.02224   0.01601  -0.0822  0.5420  1.0000
   7.100   1.1693   0.02193   0.01575  -0.0814  0.5321  1.0000
   7.200   1.1789   0.02159   0.01545  -0.0805  0.5213  1.0000
   7.300   1.1880   0.02127   0.01521  -0.0796  0.5087  1.0000
   7.400   1.1965   0.02097   0.01499  -0.0787  0.4940  1.0000
   7.500   1.2050   0.02057   0.01461  -0.0777  0.4767  1.0000
   7.600   1.2118   0.02025   0.01440  -0.0765  0.4529  1.0000
   7.700   1.2175   0.02003   0.01418  -0.0752  0.4195  1.0000
   7.800   1.2217   0.02007   0.01403  -0.0738  0.3744  1.0000
   7.900   1.2234   0.02059   0.01418  -0.0724  0.3208  1.0000
   8.000   1.2233   0.02152   0.01468  -0.0710  0.2748  1.0000
   8.100   1.2227   0.02261   0.01542  -0.0696  0.2392  1.0000
   8.200   1.2222   0.02371   0.01625  -0.0683  0.2104  1.0000
   8.300   1.2217   0.02480   0.01712  -0.0670  0.1860  1.0000
   8.400   1.2208   0.02592   0.01804  -0.0657  0.1637  1.0000
   8.500   1.2186   0.02714   0.01906  -0.0641  0.1423  1.0000
   9.000   1.2117   0.03330   0.02451  -0.0564  0.0811  1.0000