Numerical study on the coupled influence of combustor flame tube cooling holes pre-swirl and mainstream swirl on the film cooling perfomance of endwall-Reference-Cited by-同舟云学术

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Numerical study on the coupled influence of combustor flame tube cooling holes pre-swirl and mainstream swirl on the film cooling perfomance of endwall

Published:2024-07 Issue: Volume:249 Page:123269
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Li Haiwang,Zhang Jinghan,Zhou Zhiyu,Lou Yuzhu,Xie Gang

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Reference33 articles.

1. Three-dimensional flow within a turbine cascade passage;Langston;J. Eng. Power.,1977

2. Crossflows in a turbine cascade passage;Langston;J. Eng. Power.,1980

3. Film cooling effectiveness distribution on first-stage vane endwall with and without leading-edge fillets: part i—effect of leading edge geometry;Zhang;Proc. ASME Turbo Expo.,2011

4. Film cooling effectiveness distribution on first-stage vane endwall with and without leading-edge fillets: part ii—effect of incidence angle;Zhang;Proc. ASME Turbo Expo.,2011

5. On the reliability of RANS turbulence models for endwall cooling prediction;Li;Proc. ASME Turbo Expo.,2017

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