Control of secondary flows in a turbine nozzle guide vane by endwall contouring

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Shih, T I P ^a   Lin, Y L ^a   Simon, T W ^b  

^a Michigan State University   (United States)

^b University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COOLING; FINITE VOLUME METHOD; HEAT TRANSFER; NOZZLES; REYNOLDS NUMBER; SECONDARY FLOW; SHEAR FLOW; SHEAR STRESS;

COMPRESSIBLE NAVIER-STOKES; COMPUTATIONAL STUDIES; CONSERVATION EQUATIONS; FILM COOLING EFFECTIVENESS; FLUX DIFFERENCE SPLITTING; MULTIGRID ACCELERATION; SHEAR-STRESS TRANSPORT; THREE-DIMENSIONAL FLOW;

NAVIER STOKES EQUATIONS;

EID: 84956987699     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0556     Document Type: Conference Paper

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