Journal of Turbomachinery, Volume 112American Society of Mechanical Engineers - Turbomachines |
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Common terms and phrases
adverse pressure gradient aerodynamic airfoil ASME Journal axial axial compressor base pressure blade row blade surface calculation cascade centrifugal compressor compressor configuration coolant correlation 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 impeller blade impingement increase injection International Gas Turbine Journal of Engineering laminar leading edge loss Mach number mass flow mass flow rate measured midspan nondimensional nozzle Nusselt obtained parameters percent chord predicted present pressure gradient pressure ratio pressure rise pressure surface radial region relative Reynolds number rotating rotor secondary flow shown in Fig shroud spanwise speed stage stall Stanton number static pressure stator streamwise suction side suction surface temperature three-dimensional tion tip clearance total pressure trailing edge transition Transonic Turbomachinery unsteady upstream vortex vortices wake wall