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airfoil analytical calculations analytical surface pressure angle condition approximate real flow Axial distance blade surface velocities blade trailing edge boundary layer calculation boundary layer displacement boundary layer separation boundary layer thicknesses calculated boundary layer calculated loss coefficients calculated surface pressures calculation procedure camber chord location compressor blade curves effect exit flow angle Exit fluid angle experimentally measured extended Gostelow method flow and boundary flow conditions flow Experimental data initial boundary layer initial thicknesses initial turbulent boundary inlet input inviscid flow calculation Inviscid flow Experimental inviscid flow program iterative laminar boundary layer laminar separation layer and loss layer displacement thickness leading edge Lewis Research Center loss calculations measured losses measured values midspan momentum thickness outlet flow angle pressure surface separation point shown in figure Speidel stagnation point subsonic suction and pressure surface boundary layer surface pressure coefficients surface pressure distributions tion trailing edge region turbulent boundary layer z/ct