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aerodynamic airfoil analysis angle of attack ASME Journal ASME Paper Axial Compressor blade row blade surface boundary layer bow shock calculations circumferential combustion component compressor cascade computational configuration contours diffuser dihedral blades downstream vane passing effect efficiency endwall engine equations exit experimental flow angle flow field fluid gas turbine geometry grid increase inlet flow investigated isentropic Journal of Turbomachinery leading edge loading loss coefficient Mach number mass flow rate measurements method mid-span nozzle optimization outlet parameters passage vortex performance pitch plane prediction pressure distribution pressure ratio probe radial reduced region Reynolds number Riblet rotational rotor rotor blade secondary flow sensor shock wave shows simulations solver span speed stage static pressure stator struts suction side suction surface swept blade swirl total pressure loss total temperature trailing edge transonic Turbomachinery turbulence intensity upstream vane vane passing frequency variation velocity vorticity wake wall