Heat transfer characteristics of fan-shaped hole effusion cooling for a constant hole exit width – Numerical simulation and experimental validation-Reference-Cited by-同舟云学术

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Heat transfer characteristics of fan-shaped hole effusion cooling for a constant hole exit width – Numerical simulation and experimental validation

Published:2019-09 Issue: Volume:160 Page:113978
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Wei H.,Ai J.L.,Zu Y.Q.,Ding L.

Funder

United Innovation Program of Shanghai Commercial Aircraft Engine

Shanghai Municipal Commission of Economy and Informatization

Shanghai Municipal Education Commission

AECC Commercial Aircraft Engine Co., LTD

Natural Science Foundation of Shanghai

Scientific Research Foundation for the Returned Overseas Chinese Scholars

State Education Ministry

Doctoral Students Research Funding of Fudan University

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference40 articles.

1. Film cooling with injection through holes: adiabatic wall temperatures downstream of a circular hole;Goldstein;J. Eng. Power,1968

2. A review of shaped hole turbine film cooling technology;Bunker;J. heat transf.,2005

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

4. A. Kohli, D. Bogard, Effects of hole shape on film cooling with large angle injection, in: Proceedings of ASME Turbo Expo 1999, 99-GT-165, 1999.

5. Effect of hole geometry on the thermal performance of fan-shaped film cooling holes;Gritsch;ASME J. Turbomach.,2005

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3. Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations;Journal of Turbomachinery;2022-10-07

4. The Effects of Inclination Angle on the Cooling Performance of Fan-Shaped Holes under Different Blowing Ratios;2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE);2022-07-20

5. Experimental and numerical investigation of micro-scale effusion and transpiration air cooling on cascaded turbine blades;Case Studies in Thermal Engineering;2022-04

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