Effects of Inlet Swirl Angle on Flow and Heat Transfer in Contoured Turbine Nozzle Guide Vanes

American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD

Volumn 369, Issue 5, 2001, Pages 279-288

  Lin, Y L ^a   Schock, H J ^a   Shih, T I P ^a   Bunker, R S ^b  

^a Michigan State University   (United States)

^b GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW CONDITIONS; SHEAR-STRESS TRANSPORT (SST);

AERODYNAMICS; AIR ENTRAINMENT; AIRFOILS; BOUNDARY LAYERS; COMPUTER SIMULATION; COOLING; FRICTION; HEAT LOSSES; NAVIER STOKES EQUATIONS; NOZZLES; SWIRLING FLOW; TURBINES; TURBULENCE; VANE PUMPS; VISCOSITY;

HEAT TRANSFER;

EID: 0347028132     PISSN: 02725673     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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