Conjugate heat transfer effects on a realistic film-cooled turbine vane

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

Volumn 5 A, Issue , 2003, Pages 361-371

  Heidmann, James D ^a   Kassab, Alain J ^b   Divo, Eduardo A ^b   Rodriguez, Franklin ^b   Steinthorsson, Erlendur ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b UNIVERSITY OF CENTRAL FLORIDA   (United States)

^c A and E Consulting   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FILM COOLING; STAGNATION; STANTON NUMBER;

BOUNDARY ELEMENT METHOD; DENSITY (SPECIFIC GRAVITY); HEAT CONDUCTION; HEAT CONVECTION; HEAT FLUX; NICKEL ALLOYS; PRANDTL NUMBER; SILICON NITRIDE; SPECIFIC HEAT; TURBOMACHINE BLADES; VANE PUMPS;

GAS TURBINES;

EID: 0346327061     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38553     Document Type: Conference Paper

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