Experimental investigation on the leading edge film cooling of cylindrical and laid-back holes with different hole pitches
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference30 articles.
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2. Stagnation region gas film cooling for turbine blade leading edge applications;Luckey;AIAA J. Aircraft,1977
3. Surface injection effect on mass transfer from a cylinder in crossflow: a simulation of film cooling in the leading edge region of a turbine blade;Karni;ASME J. Turbomach.,1990
4. Influence of high mainstream turbulence on leading edge film cooling heat transfer;Mehendale;ASME J. Turbomach.,1992
5. Reynolds number effect on leading edge film effectiveness and heat transfer coefficient;Mehendale;Int. J. Heat Mass Transfer,1993
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