Film-cooling from holes with expanded exits: A comparison of computational results with experiments

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1997, Pages

  Giebert, D ^a   Gritsch, M ^a   Schulz, A ^a   Wittig, S ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CODES (SYMBOLS); FLOW FIELDS; GAS TURBINES; GEOMETRY; HEAT TRANSFER; NAVIER STOKES EQUATIONS; WALL FUNCTION;

ADIABATIC FILM COOLING EFFECTIVENESS; COMPUTATIONAL RESULTS; FILM COOLING HOLE; FLOW FIELD MEASUREMENT; FUNCTION APPROACHES; NAVIER-STOKES CODE; NUMERICAL RESULTS; PREDICTIVE CAPABILITIES;

COOLING;

EID: 84973667636     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-163     Document Type: Conference Paper

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