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aerofoil airfoil alloy analysis ASME ASME Journal axial compressor boundary layer brush seal calculated cascade cavity coating coefficient coefficient of lift cogeneration component compressor computational coolant jets Copyright Copyright Clearance Center cycle effect endwall engine equation exit experimental fatigue fillet film cooling frequency gas turbine grid HASTELLOY heat high lift holes HRSG increase injection inlet fogging isentropic surface leading edge linear loading loss LP turbine Mach number measurements mesh level micro gas turbine microstructure midspan nozzle operating oxidation parameters passage vortex performance predicted pressure gradient pressure side pressure surface separation pulse detonation Pulse Detonation Engine ratio reduced region Reynolds number rotor secondary flow shear shear stress showerhead shown in Figure shows simulation spanwise specimen stagnation stagnation pressure stator strain stress suction surface superalloy TBCs temperature thermal conductivity thickness trailing edge turbofan Turbomachinery unsteady upstream vane velocity