Effects of surface roughness on heat transfer and aerodynamic performance of turbine airfoils

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1997, Pages

  Abuaf, N ^a   Bunker, R S ^a   Lee, C P ^b  

^a GENERAL ELECTRIC COMPANY   (United States)

^b GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; AIRFOILS; DRAG; EFFICIENCY; ENGINES; FINISHING; FRICTION; GAS TURBINES; HEAT TRANSFER COEFFICIENTS; POLISHING; REYNOLDS NUMBER; SURFACE ROUGHNESS; SURFACE TREATMENT; TURBINE COMPONENTS;

AERO-DYNAMIC PERFORMANCE; COOLING REQUIREMENTS; ENGINE CONDITIONS; ENGINE PERFORMANCE; IMPROVE PERFORMANCE; LOCAL HEAT TRANSFER COEFFICIENT; LOCAL SKIN-FRICTION COEFFICIENT; TRANSIENT TECHNIQUES;

HEAT TRANSFER;

EID: 84973596417     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-010     Document Type: Conference Paper

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