Discharge coefficient measurements of film-cooling holes with expanded exits

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1997, Pages

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

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; COOLING; GEOMETRY; HEAT TRANSFER; MACH NUMBER;

CYLINDRICAL HOLES; DISCHARGE COEFFICIENTS; EXPANDED HOLES; FANSHAPED HOLES; FILM COOLING HOLE; FLOW CONDITION; HOLE GEOMETRY; PRESSURE RATIO;

GAS TURBINES;

EID: 84973598672     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-165     Document Type: Conference Paper

References (19)

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12. Kline, S. and F. McClintock (1953). Describing Uncertainties in Single-Sample Experiments . Mechanical Engineering, Vol. 75, pp. 3-8.
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17. Thole, K., M. Gritsch, A. Schulz, and S. Wittig (1996). Flowfield Measurements for Film-Cooling Holes with Expanded Exits. ASME Paper 96-GT-174.
18. Thole, K., M. Gritsch, A. Schulz, and S. Wittig (1997). Effect of a Crossflow at the Entrance to a Film- Cooling Hole. Accepted for publication in the ASME Journal of Fluids Engineering.
19. Wittig, S., A. Schulz, M. Gritsch, and K. Thole (1996). Transonic Film-Cooling Investigations: Effects of Hole Shapes and Orientations. ASME Paper 96-GT- 222.