Flow field simulations of a gas turbine combustor

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2001, Pages

  Barringer, M D ^a   Richard, O T ^a   Walter, J P ^a   Stitzel, S M ^a   Thole, K A ^a  

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; FLOW FIELDS; GAS TURBINES; ROCKET NOZZLES; TURBINE COMPONENTS;

COMBUSTOR LINERS; FLOW FIELD SIMULATION; GAS TURBINE COMBUSTOR; NEAR-WALL REGION; NOZZLE GUIDE VANES; TUNNEL SECTIONS; TURBULENCE LEVEL; TURBULENT BOUNDARY LAYERS;

COMBUSTORS;

EID: 84905728364     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0170     Document Type: Conference Paper

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