XFOIL         Version 6.94
  
 Calculated polar for: Rhode St. Genese 36                             
  
 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   0.6029   0.01659   0.00812  -0.0611  0.3129  0.1952
   0.500   0.6469   0.01712   0.00876  -0.0594  0.3140  0.2493
   1.000   0.8406   0.01743   0.01103  -0.0877  0.3153  1.0000
   1.500   0.8630   0.01823   0.01184  -0.0821  0.3149  1.0000
   2.000   0.8818   0.01914   0.01279  -0.0761  0.3146  1.0000
   2.500   0.9014   0.02018   0.01388  -0.0706  0.3145  1.0000
   3.000   0.9208   0.02143   0.01518  -0.0653  0.3136  1.0000
   3.500   0.9376   0.02287   0.01669  -0.0598  0.3126  1.0000
   4.000   0.9432   0.02497   0.01892  -0.0533  0.3089  1.0000
   4.500   0.9274   0.02801   0.02214  -0.0447  0.3055  1.0000
   5.000   0.9103   0.03189   0.02621  -0.0373  0.3029  1.0000
   5.500   0.8789   0.03691   0.03142  -0.0301  0.3024  1.0000
   6.000   0.8578   0.04239   0.03705  -0.0255  0.3023  1.0000
   6.500   0.8322   0.04905   0.04384  -0.0222  0.3031  1.0000
   7.000   0.8168   0.05617   0.05105  -0.0206  0.3031  1.0000
   7.500   0.7840   0.06674   0.06174  -0.0202  0.3018  1.0000