Coupled Heat Transfer Simulation of a High-pressure Turbine Nozzle Guide Vane

Chinese Journal of Aeronautics

Volumn 22, Issue 3, 2009, Pages 230-236

  Qiang, Wang ^a   Zhaoyuan, Guo ^a   Chi, Zhou ^a   Guotai, Feng ^a   Zhongqi, Wang ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

boundary layer flow; heat transfer; transition flow; turbines; turbulence model

Indexed keywords

A-THERMAL; ABU-GHANNAM AND SHAW MODELS; ALGEBRAIC MODELS; COUPLED HEAT TRANSFER; COUPLED SOLVER; HIGH PRESSURE TURBINE; OPERATING CONDITION; TRANSITION ZONES; TURBINE VANES; TURBULENT ZONES;

AERODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; ENGINES; FLUID DYNAMICS; HEAT EXCHANGERS; HEAT TRANSFER; NASA; SIMULATORS; THERMAL LOAD; THREE DIMENSIONAL; TRANSITION FLOW; TURBINES;

TURBULENCE MODELS;

EID: 67649224926     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(08)60092-8     Document Type: Article

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