
    XFLR5_v2.007

 Calculated polar for: E423

 1 1 Reynolds number fixed          Mach number fixed         

 xtrf =   1.000 (top)        1.000 (bottom)
 Mach =   0.000     Re =     0.300 e 6     Ncrit =   9.000

  alpha     CL        CD       CDp       CM    Top Xtr Bot Xtr   Cpmin    Chinge
 ------- -------- --------- --------- -------- ------- ------- -------- ---------


