Effects of gap leakage on fluid flow in a contoured turbine nozzle guide vane

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Lin, Y L ^a   Shih, T I P ^a   Chyu, M K ^b   Bunker, R S ^c  

^a Michigan State University   (United States)

^b CARNEGIE MELLON UNIVERSITY   (United States)

^c GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FINITE VOLUME METHOD; HEAT TRANSFER; NAVIER STOKES EQUATIONS; NOZZLES; REYNOLDS NUMBER; SECONDARY FLOW; SHEAR FLOW; SHEAR STRESS;

BACKWARD FACING STEP; COMPRESSIBLE NAVIER-STOKES; COMPUTATIONAL STUDIES; CONSERVATION EQUATIONS; FLUX DIFFERENCE SPLITTING; MULTIGRID ACCELERATION; SHEAR-STRESS TRANSPORT; THREE-DIMENSIONAL FLOW;

FLOW OF FLUIDS;

EID: 84922585383     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0555     Document Type: Conference Paper

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