Numerical 3-D conjugate flow and heat transfer investigation of a transonic convection-cooled thermal barrier coated turbine guide vane with reduced cooling fluid mass flow

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 5 A, Issue , 2003, Pages 279-286

  Bohn, Dieter E ^a   Tümmers, Christian ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMICS; THERMAL BARRIER; TURBINE INLET TEMPERATURES;

BOUNDARY CONDITIONS; COMPRESSORS; COMPUTER SIMULATION; FLOW OF FLUIDS; GAS TURBINES; HEAT TRANSFER; MASS TRANSFER; NOZZLES; TEMPERATURE DISTRIBUTION; THERMAL CONDUCTIVITY; THERMAL LOAD; THERMAL STRESS; THERMOANALYSIS;

TRANSONIC AERODYNAMICS;

EID: 0346335508     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38431     Document Type: Conference Paper

References (13)

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