Experimental investigation on the effects of rotation and the blowing ratio on the leading-edge film cooling of a twist turbine blade

Author:

Li Hai-wang,Han Feng,Ma Yi-wen,Wang Hai-chao,Zhou Zhi-yu,Tao Zhi

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference23 articles.

1. Gas turbine heat transfer and cooling technology;Han;Epfl,2014

2. Stagnation film cooling and heat transfer, including its effect within the hole pattern;Mick;J. Turbomach.,1988

3. Michael W. Cruse, Ushio M. Yuki, David G. Bogard, Investigation of various parametric influences on leading edge film cooling, in: ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition, 1997, pp. V003T09A058–V003T09A058.

4. Detailed film cooling measurements on a cylindrical leading edge model: effect of free-stream turbulence and coolant density;Ekkad;J. Turbomach.,1998

5. Three-dimensional flow and heat transfer calculations of film cooling at the leading edge of a symmetrical turbine blade model;Lakehal;Int. J. Heat Fluid Flow,2001

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