Trajectory and effectiveness of film cooling in endwall crossflow-Reference-Cited by-同舟云学术

Trajectory and effectiveness of film cooling in endwall crossflow

Published:2022-09 Issue: Volume:128 Page:107795
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chen Ziyu,Su Xinrong^ORCID,Yuan Xin

Funder

National Natural Science Foundation of China

Tsinghua University

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Measurement and calculation of turbine cascade endwall pressure and shear stress;Holley;J. Turbomach.,2008

2. Geometrical parameter effects on film-cooling effectiveness of rectangular diffusion holes;An;J. Turbomach.,2017

3. Large eddy simulation of unsteady turbulent flow structures and film-cooling effectiveness in a laidback fan-shaped hole;Zamiri;Aerosp. Sci. Technol.,2020

4. Multi-objective optimization of round-to-slot film cooling holes on a flat surface;Huang;Aerosp. Sci. Technol.,2020

5. A review of shaped hole turbine filmcooling technology;Bunker;J. Heat Transf.,2005

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3. Large Eddy simulation in optimizing trench configuration to improve cooling effectiveness of a laidback fan-shaped hole;International Communications in Heat and Mass Transfer;2023-10

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