Influence of Large Wake Disturbances Shed From the Combustor Wall on the Leading Edge Film Cooling
Author:
Affiliation:
1. Mem. ASME Osney Thermo-Fluids Laboratory, Department of Engineering Science, Oxford University, Southwell Building, Osney Mead, Oxford OX2 0DP, UK e-mail:
2. The Boston Consulting Group GmbH, Am Stadttor 1, Dusseldorf 40219, Germany e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4026803/6161871/gtp_136_08_081503.pdf
Reference37 articles.
1. Stagnation Film Cooling and Heat Transfer, Including Its Effect Within the Hole Pattern;ASME J. Turbomach.,1988
2. Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer;ASME J. Turbomach.,1992
3. Cruse, M. W., Yuki, U. M., and Bogard, D. G., 1997, “Investigation of Various Parametric Influences on Leading Edge Film Cooling,” ASME Paper No. 97-GT-296.
4. Effect of Periodic Wake Passing on Film Effectiveness of Discrete Cooling Holes Around the Leading Edge of a Blunt Body;ASME J. Turbomach.,1997
5. Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade;ASME J. Turbomach.,1998
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