Effect of squealer cavity depth and oxidation on turbine blade tip heat transfer

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2001, Pages

  Bunker, Ronald S ^a   Bailey, Jeremy C ^a  

^a GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; HEAT TRANSFER COEFFICIENTS; MACH NUMBER; REYNOLDS NUMBER; TURBINES; TURBOMACHINE BLADES;

CONVECTIVE HEAT TRANSFER COEFFICIENT; HEAT TRANSFER DISTRIBUTIONS; HIGH PRESSURE TURBINE BLADE; SURFACE HEAT TRANSFER; SURFACE INFORMATION; TIP HEAT TRANSFER; TURBINE BLADE TIP; TURBULENCE INTENSITY LEVEL;

AERODYNAMICS;

EID: 84905758104     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0155     Document Type: Conference Paper

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