Flowfield measurements for film-cooling holes with expanded exits

Journal of Turbomachinery

Volumn 120, Issue 2, 1998, Pages 327-336

  Thole, K ^a,b   Gritsch, M ^a   Schulz, A ^a   Wittig, S ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

^b University of Wisconsin Madison   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 11644284181     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841410     Document Type: Article

References (16)

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3. Garg, V., and Gaugler, R, 1995, “Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades,” ASME Paper No. 95-GT-275.
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11. Schlichting, H., 1979, Boundary Layer Theory, McGraw-Hill, New York.
12. Sen, B., Schmidt, D. L., and Bogard, D. G., 1996, “Film Cooling With Compound Angle Holes: Heat Transfer,” ASME Journal of Turbomachinery, Vol. 118, pp. 800-806.
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