Effect of internal coolant crossflow orientation on the discharge coefficient of shaped film-cooling holes

Journal of Turbomachinery

Volumn 122, Issue 1, 2000, Pages 146-152

  Gritsch, M ^a,b   Saumweber, C ^a   Schulz, A ^a   Wittig, S ^a   Sharp, E ^a,c  

^a UNIVERSITY OF KARLSRUHE   (Germany)

^b ABB CORPORATE RESEARCH   (Switzerland)

^c Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CROSS FLOWS; CYLINDRICAL HOLES; DISCHARGE COEFFICIENTS; ENGINE LIKE CONDITIONS; FANSHAPED HOLES; FILM COOLING; FLOW CONDITION; FLOW DIRECTION; HOLE AXIS; HOLE GEOMETRY; HOT GAS; PERPENDICULAR ORIENTATION; PRESSURE RATIO;

AERODYNAMICS; COOLANTS; MACH NUMBER;

GEOMETRY;

BOUNDARY LAYER; COOLING; FILM; FLOW; PLATE;

EID: 0034069823     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555436     Document Type: Article

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