Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference33 articles.
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4. M.W. Cruse, U.M. Yuki, D.G. Bogard, Investigation of various parametric influences on leading edge film cooling, ASME Paper 97-GT-296, 1997.
5. Combined effect of grid turbulence and unsteady wake on film effectiveness and heat transfer coefficient of a gas turbine blade with air and CO2 Film Injection;Ekkad;ASME J. Turbomach.,1997
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