Detailed showerhead cooling effectiveness measurements on the notched leading-edge surface: Effect of freestream turbulence and density ratio-Reference-Cited by-同舟云学术

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Detailed showerhead cooling effectiveness measurements on the notched leading-edge surface: Effect of freestream turbulence and density ratio

Published:2022-06 Issue: Volume:135 Page:106142
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Ye Lin,Liu Cunliang,Li Bingran,Zhu Andong

Funder

National Major Science and Technology Projects of China

Science Fund for Distinguished Young Scholars of Tianjin

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics

Reference29 articles.

1. Turbine blade showerhead film cooling: influence of hole angle and shaping;Lu;Int. J. Heat Fluid Fl.,2007

2. Effect of jet pulsation and duty cycle on film cooling from a single jet on a leading edge model;Ekkad;ASME J. Turbomach.,2006

3. Effect of coolant–mainstream blowing ratio on leading-edge film cooling flow and heat transfer-LES investigation;Rozati;Int. J. Heat Fluid Fl.,2008

4. Experimental evaluations of the relative contributions to overall effectiveness in turbine blade leading edge cooling;Bryant;ASME J. Turbomach.,2019

5. Aspects of vane film cooling with high turbulence: part II—adiabatic effectiveness;Ames;ASME J. Turbomach.,1998

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