Heat transfer and flow on the first stage blade tip of a power generation gas turbine part 1: Experimental results

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Bunker, Ronald S ^a   Bailey, Jeremy C ^a   Ameri, Ali A ^b  

^a GE GLOBAL RESEARCH   (United States)

^b AYT Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; COMPUTATIONAL GEOMETRY; GAS TURBINES; HEAT CONVECTION; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; LIQUID CRYSTALS; MACH NUMBER; PRESSURE DISTRIBUTION; RESPIRATORY MECHANICS; REYNOLDS NUMBER; TURBOMACHINE BLADES; TURBULENCE;

COMPUTATIONAL STUDIES; CONVECTIVE HEAT TRANSFER COEFFICIENT; DISTRIBUTION MEASUREMENT; HEAT TRANSFER AND FLOWS; HEAT TRANSFER COEFFICIENT DISTRIBUTION; HIGH PRESSURE TURBINE BLADE; SURFACE INFORMATION; TURBULENCE INTENSITY LEVEL;

TURBINE COMPONENTS;

EID: 84928491984     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-169     Document Type: Conference Paper

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