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adverse pressure gradient aerodynamic airfoil ASME Journal axial axial compressor base pressure blade row blade surface calculated cascade centrifugal compressor compressor computed configuration coolant density diameter downstream effect efficiency endwall equation exit experimental film cooling flow angle flow coefficient flow field flow rate fluid free-stream Gas Turbine geometry heat flux heat transfer coefficient holes impeller blade impingement increase injection Journal of Engineering laminar leading edge loss Mach number mass flow mass flow rate measured midspan nondimensional nozzle Nusselt obtained parameters passage percent chord predicted present pressure gradient pressure ratio pressure rise pressure surface radial region relative Reynolds number rotating rotor rotor blade secondary flow shown in Fig spanwise speed stage stall static pressure stator streamwise suction side suction surface temperature three-dimensional tion tip clearance total pressure trailing edge transition Transonic Turbomachinery unsteady upstream velocity vortex wake wall