Effects of pressure gradient on film cooling effectiveness from two rows of simple and compound angle holes in combination
Author:
Publisher
Elsevier BV
Subject
Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment
Reference9 articles.
1. Interaction between embedded vortices and injectant from film cooling holes with compound angle orientations in a turbulent boundary layer;Ligrani;ASME J. Turbomach.,1994
2. Ekkad SV, Zapta D, Han J. Film cooling over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method, ASME Paper 95-GT-11, 1995
3. Film cooling with compound angle holes: adiabatic effectiveness;Schmidt;ASME J. Turbomach.,1996
4. Film cooling from two rows of holes inclined in the streamwise and spanwise directions;Jubran;ASME J. Eng. Gas Turbines Power,1985
5. Film cooling in the presence of mainstream pressure gradients;Teekarama;ASME J. Turbomach.,1991
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