Compressible Pressure Coefficients Plot, Mach = 0.6, With Cp Critical and Normal Sho - - Lower Surface Compressible Pressure Coefficient 1.8 Surface Compressible Pressure Coefficient X 0.333 Pressure Coefficient 1.6 Y 1.49149 shock Lift Loss 1.4 11 1 1 14141 1 1 1 1 1 1 14 1 1 1 1 1 1 1 1 1 1 1:.. X 0.333 X 0.644 1.2 Y 1.1079 Y 1.1079 Negative Pressure Coefficient 0.8 0.6 0.4 0.2 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 Chord FractionCL = 0.5 (3.1X (1-X) + 1.3X . (1-X) 2.5 2 dx = 0.6285