Paper

adiabatic angle ASME averaged bearing blade blowing ratio boundary layer calculated changes compared compressor computational configuration console contours coolant crossflow decrease diameter direction discharge coefficient discussion distance distribution downstream edge effectiveness efficiency ejection endwall energy engine equations exit experimental experiments field Figure film cooling film cooling hole film hole flow rate fluid flux gas turbine geometry grid heat transfer coefficient higher impingement increase injection inlet internal Journal leading loss lower Mach number mainstream mass flow mean measured momentum nozzle obtained operating orientation parameters passage performance plane plate prediction present pressure pressure ratio pressure side reduced region relative Reynolds number rotor seal secondary shown shows side single slot steam surface Table temperature thermal turbulence values velocity vortex wall