Large eddy simulations of the turbine vane pressure side film cooling flows of cylindrical and fan-shaped holes with a saw-tooth plasma actuator-Reference-Cited by-同舟云学术

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Large eddy simulations of the turbine vane pressure side film cooling flows of cylindrical and fan-shaped holes with a saw-tooth plasma actuator

Published:2024-09 Issue: Volume: Page:124404
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Li Guozhan,Zhang Shuang,Shen Zhou,Zhang Hongjun

Funder

China Postdoctoral Science Foundation

Fundamental Research Funds for the Provincial Universities of Zhejiang Province

National Natural Science Foundation of China

Zhejiang Province Natural Science Foundation

Publisher

Elsevier BV

Reference30 articles.

1. Investigation on the showerhead film cooling of the turbine vane considering combustor swirling outflow;Wang;Appl. Therm. Eng.,2023

2. Film cooling and aerodynamic loss performance of turbine vanes with fan-shaped and wave-trenched holes;Chen;Appl. Therm. Eng.,2023

3. Effects of hole geometry and density on three-dimensional film cooling;Goldstein;Int. J. Heat Mass Transf.,1974

4. Film cooling: breaking the limits of diffusion shaped holes;Bunker;Heat Transf. Res.,2009

5. P. Renze, W. Schroeder, M. Meinke, Hole shape comparison for film cooling flows using large eddy simulations, AIAA J.

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