Experimental and numerical investigation on middle passage gap leakage with different mass flow rate and injection angle on turbine endwall-Reference-Cited by-同舟云学术

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Experimental and numerical investigation on middle passage gap leakage with different mass flow rate and injection angle on turbine endwall

Published:2024-10 Issue: Volume:109 Page:109533
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Song Yu,Liu Zhao^ORCID,Zhang Weixin,Ding Yuqiang,Feng Zhenping

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Reference23 articles.

1. Effect of midpassage gap, endwall misalignment, and roughness on endwall film-cooling;Cardwell;J. Turbomach.,2005

2. Turbine blade platform film cooling with simulated swirl purge flow and slashface leakage conditions;Chen;J. Turbomach.,2016

3. Turbine vane endwall film cooling with slashface leakage and discrete hole configuration;Chowdhury;J. Turbomach.,2017

4. Computational study of a midpassage gap and upstream slot on vane endwall film-cooling;Hada;J. Turbomach.,2010

5. Effect of inlet conditions on endwall secondary flows;Hermanson;J. Propul. Power,2000

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