Film cooling effectiveness and heat transfer on the trailing edge cut-back of gas turbine airfoils with various internal cooling designs

Proceedings of the ASME Turbo Expo

Volumn 3 PART A, Issue , 2005, Pages 87-96

  Martini, P ^a   Schulz, A ^a   Bauer, H J ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ADIABATIC FILMS; FILM COOLING; INTERNAL COOLING DESIGN; TRAILING EDGE;

AIRFOILS; COOLANTS; COOLING; GAS TURBINES; REYNOLDS NUMBER; TURBULENCE;

HEAT TRANSFER;

EID: 27744454459     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2005-68083     Document Type: Conference Paper

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