Influence of turbine blade leading edge shape on film cooling with cylindrical holes
Author:
Funder
Texas A and M University
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference28 articles.
1. Gas Turbine Heat Transfer and Cooling Technology;Han,2012
2. Stagnation film cooling and heat transfer, including its effect within the hole pattern;Mick;ASME. J. Turbomach.,1988
3. Detailed film cooling measurement on a cylindrical leading edge model: effect of free-stream turbulence and coolant density;Ekkad;ASME J. Turbomach.,1998
4. Large Eddy simulation of leading edge film cooling—Part II: Heat transfer and effect of blowing ratio;Rozati;ASME. J. Turbomach.,2008
5. Effect of coolant–mainstream blowing ratio on leading edge film cooling flow and heat transfer – LES investigation;Rozati;Int. J. Heat Fluid Flow,2008
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