Effect of continuous or discrete shock wave generators on supersonic film cooling-Reference-Cited by-同舟云学术

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Effect of continuous or discrete shock wave generators on supersonic film cooling

Published:2017-05 Issue: Volume:108 Page:770-783
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:

Peng Wei,Sun Xiaokai,Jiang Peixue,Wang Jie

Funder

National Natural Science Foundation of China

Creative Research Groups of the NSFC

National S&T Major Project

Publisher

Elsevier BV

Subject

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

Reference28 articles.

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

2. Film cooling effectiveness and heat transfer coefficient distributions around diffusion shaped holes;Yu;J. Heat Transfer,2002

3. Influence of cooling-gas properties on film-cooling effectiveness in supersonic flow;Keller;J. Spacecraft Rockets,2015

4. Numerical analysis of supersonic film cooling in supersonic flow in hypersonic inlet with isolator;Zhang;Adv. Mech. Eng.,2014

5. Film cooling in laminar and turbulent supersonic flows;Hombsch;J. Spacecraft Rockets,2013

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