Perspectives in modeling film cooling of turbine blades by transcending conventional two-equational turbulence models

Journal of Turbomachinery

Volumn 124, Issue 3, 2002, Pages 472-484

  Azzi, A ^a   Lakehal, D ^a  

^a ETH ZURICH   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRA; ANISOTROPY; BOUNDARY LAYERS; COOLING; DIFFUSION; HEAT TRANSFER; NONLINEAR EQUATIONS; STATISTICS; STRAIN; STRESSES; TURBOMACHINE BLADES; TURBULENCE; VISCOSITY; VORTEX FLOW;

TURBINE BLADES;

TURBINES;

BLADE; FILM COOLING; TURBINE; TURBULENCE;

EID: 0036648336     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1485294     Document Type: Article

References (27)

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4. Predictions of a film cooling jet in cross-flow with different turbulence models
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6. 3D calculations of the flow field around a turbine blade with film cooling injection near the leading edge
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