Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade-Reference-Cited by-同舟云学术

Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade

Published:2018-12 Issue: Volume:127 Page:856-869
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

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

Publisher

Elsevier BV

Subject

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

Reference27 articles.

1. Film cooling;Goldstein;Adv. Heat Transfer,1971

2. Gas Turbine Heat Transfer and Cooling Technology;Han,2012

3. Stagnation region gas film cooling for turbine blade leading edge applications;Luckey;J. Aircraft,1976

4. Detailed film cooling measurements on a cylindrical leading edge model: effect of free-stream turbulence and coolant density;Ekkad;J. Turbomach.,1997

5. Leading edge film cooling heat transfer with high free stream turbulence using a transient liquid crystal image method;Ou;Int. J. Heat Fluid Fl.,2001

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