Film cooling comparison of shaped holes among the pressure surface, the suction surface and the leading edge of turbine vane-Reference-Cited by-同舟云学术

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Film cooling comparison of shaped holes among the pressure surface, the suction surface and the leading edge of turbine vane

Published:2023-01 Issue: Volume:219 Page:119343
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Jiang Yan,Li Haiwang,Liu Runzhou,Tao Zhi,Zhou Zhiyu

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference35 articles.

1. Film Cooling: Breaking the Limits of Diffusion Shaped Holes;S.;Heat Transf. Res.,2010

2. Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio;Sinha;J. Turbomach.,1991

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

4. Large eddy simulation of film cooling flow from a fanshaped hole;Wang;Appl. Therm. Eng.,2018

5. Experimental investigation of film cooling effectiveness on a gas turbine blade pressure surface with diffusion slot holes;Yu;Appl. Therm. Eng.,2020

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of aerodynamic loss mechanism on turbine leading edge with slot film cooling based on entropy analysis;International Journal of Thermal Sciences;2025-01

2. Experimental and numerical investigations on film cooling performances with spiral-channel holes for a turbine vane;Applied Thermal Engineering;2024-11

3. Film cooling effectiveness investigation of diffusion slot holes on a turbine guide vane leading edge;International Communications in Heat and Mass Transfer;2024-11

4. Numerical investigation of flow and heat transfer on turbine guide vane leading edge slot film cooling;Energy;2024-11

5. A total three-dimensional evaluation method to analyze the loss mechanism of film cooling on turbine guide vane;Applied Thermal Engineering;2024-09

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