XFOIL         Version 6.94
  
 Calculated polar for: Marsden                                         
  
 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
 ------- -------- --------- --------- -------- ------- -------
   0.000   1.0877   0.03355   0.02808  -0.2036  0.4407  0.5933
   0.500   1.1340   0.03516   0.02966  -0.2026  0.4395  0.6197
   1.500   0.8697   0.05944   0.05500  -0.1720  0.4254  0.6103