Proceedings of the ASME Turbo Expo 2002, Volume 5, Part 2American Society of Mechanical Engineers, 2002 - Aircraft gas-turbines |
Common terms and phrases
aerodynamic airfoil analysis APNASA ASME ASME Paper averaged axial chord Axial Compressor blade row blade surface boundary layer bow shock calculations circumferential computational configuration contours diffuser downstream vane effect efficiency endwall engine equations exit experimental Figure flow field fluid gas turbine geometry grid impeller increase inlet flow interaction investigated isentropic Journal of Turbomachinery leading edge loading loss coefficient Mach number mass flow rate measurements mesh method mid-span midspan nozzle optimization parameters particle passage vortex performance pitch pitchwise plane predicted pressure distribution pressure field pressure ratio prismatic blading probe radial reduced region Reynolds number Riblet rotating rotor rotor blade secondary flow sensor shown shows simulations solver spacing span speed stage static pressure stator struts suction side suction surface swept blade swirl three-dimensional total pressure loss trailing edge transonic Turbomachinery turbulence intensity turbulence model variation velocity vorticity wall