Heat transfer coefficients on the squealer tip and near tip regions of a gas turbine blade with single or double squealer

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

Volumn 5 A, Issue , 2003, Pages 681-690

  Kwak, Jae Su ^a   Ahn, Jaeyong ^a   Han, Je Chin ^a   Lee, C Pang ^b   Bunker, Ronald S ^c   Boyle, Robert ^d   Gaugler, Raymond ^d  

^a Texas AandM University   (United States)

^b GE AVIATION   (United States)

^c GE GLOBAL RESEARCH   (United States)

^d NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EXIT VELOCITY; RECOVERY TEMPERATURE;

BOUNDARY LAYERS; GAS TURBINES; GEOMETRY; HEAT TRANSFER; LEAKAGE (FLUID); REYNOLDS NUMBER; TRANSIENTS;

TURBOMACHINE BLADES;

EID: 0346965281     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38907     Document Type: Conference Paper

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