Heat transfer coefficient and film-cooling effectiveness on the squealer tip of a gas turbine blade

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 3 B, Issue , 2002, Pages 1073-1082

  Kwak, Jae Su ^a   Han, Je Chin ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLOWING RATIO; FILM COOLING; GAS TURBINE BLADE; SQUEALER; TURBULENCE INTENSITY LEVEL;

AIRCRAFT ENGINES; COOLING; FILMS; HEAT TRANSFER; MATHEMATICAL MODELS; PRESSURE EFFECTS; REYNOLDS NUMBER; TURBOMACHINE BLADES; TURBULENCE;

GAS TURBINES;

EID: 0036995334     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30555     Document Type: Conference Paper

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