Computational prediction of heat transfer to gas turbine nozzle guide vanes with roughened surfaces

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 4, Issue , 1996, Pages

  Guo, S M ^a   Jones, T V ^a   Lock, G D ^b   Dancer, S N ^c  

^a UNIVERSITY OF OXFORD   (United Kingdom)

^b UNIVERSITY OF BATH   (United Kingdom)

^c ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

GAS TURBINES; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; LIQUID CRYSTALS; NOZZLES; REYNOLDS NUMBER; SHEAR FLOW; SURFACE ROUGHNESS; TURBINE COMPONENTS; WALL FUNCTION;

COMPUTATIONAL CODES; COMPUTATIONAL PREDICTIONS; GAS TURBINE NOZZLES; MOMENTUM EQUATION; ROUGHENED SURFACES; SURFACE SHEAR FLOW; THIN-FILM GAUGES; TRANSIENT LIQUID CRYSTAL TECHNIQUE;

NAVIER STOKES EQUATIONS;

EID: 84923879006     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-388     Document Type: Conference Paper

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