XFOIL         Version 6.94
  
 Calculated polar for: UNIVERSITY OF GLASGOW GU25-5(11                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.080     Re =     0.300 e 6     Ncrit =   9.000
  
  alpha     CL        CD       CDp       CM    Top_Xtr Bot_Xtr
 ------- -------- --------- --------- -------- ------- -------
   0.000   0.5340   0.01389   0.00479  -0.1088  0.5535  0.2892
   0.500   0.2939   0.02705   0.01524  -0.0670  0.0185  0.0431
   1.000   0.3308   0.02800   0.01625  -0.0658  0.0594  0.0490
   1.500   0.3616   0.02966   0.01764  -0.0644  0.0362  0.0370