XFOIL         Version 6.94
  
 Calculated polar for: LWK 80-150/K25                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.080     Re =     0.450 e 6     Ncrit =   9.000
  
  alpha     CL        CD       CDp       CM    Top_Xtr Bot_Xtr
 ------- -------- --------- --------- -------- ------- -------
   1.000   0.2591   0.01045   0.00232  -0.0303  0.6225  0.0733
   2.500   0.0906   0.01426   0.00383   0.0379  0.0436  0.1062
   3.000   0.0751   0.01220   0.00355   0.0515  0.0302  0.6207
   3.500   0.1459   0.01479   0.00424   0.0479  0.0092  0.1171