A Numerical Investigation of Heat Transfer Characteristics with Varying Film Cooling Hole Shapes for Gas Turbine Blade Cooling-Reference-Cited by-同舟云学术

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A Numerical Investigation of Heat Transfer Characteristics with Varying Film Cooling Hole Shapes for Gas Turbine Blade Cooling

Published:2022-06-01 Issue:6 Volume:39 Page:443-450
ISSN:1225-9071
Container-title:Journal of the Korean Society for Precision Engineering
language:en
Short-container-title:KSPE

Author:

Park Chan Hyeok,Tamang Sajan,Kwon Hwabhin,Choi Jaemun,Park Heesung^ORCID

Funder

Ministry of Trade, Industry and Energy

Korea Institute of Energy Technology Evaluation and Planning

Publisher

Korean Society of Precision Engineering

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Safety, Risk, Reliability and Quality

Reference13 articles.

1. Gas Turbine Working Principles

2. Film Cooling

3. Surrogate based optimization of a laidback fan-shaped hole for film-cooling

4. Numerical investigation of adiabatic film cooling effectiveness through compound angle variations

5. Improvement on shaped-hole film cooling effectiveness by integrating upstream sand-dune-shaped ramps

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