Numerical investigation of adiabatic film cooling effectiveness through compound angle variations-Reference-Cited by-同舟云学术

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Numerical investigation of adiabatic film cooling effectiveness through compound angle variations

Published:2020-08-19 Issue:10 Volume:78 Page:595-618
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Tamang Sajan¹,Kwon Hwabhin¹,Choi Jaehun¹,Ligrani Phillip²,Lee Je-Hyun³,Jung Yeon-Gil³,Park Heesung¹

Affiliation:

1. Graduate School of Mechanical Engineering, Changwon National University, Gyeongsangnam-do, South Korea

2. Department of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, USA

3. School of Material Science, Changwon National University, Gyeongsangnam-do, South Korea

Funder

Korea Institute of Energy Technology Evaluation and Planning (KETEP) Program

Ministry of Trade, Industry and Energy of the Republic of Korea

National Research Foundation of Korea

Publisher

Informa UK Limited

Subject

Condensed Matter Physics,Numerical Analysis

Link

https://www.tandfonline.com/doi/pdf/10.1080/10407782.2020.1803600

Reference26 articles.

1. Combined Cycle Driven Efficiency for Next Generation Nuclear Power Plants

2. Film Cooling

3. Experimental Thermal Field Measurements of Film Cooling Above the Suction Surface of a Turbine Vane

4. Film cooling effectiveness from trenched shaped and compound holes

5. Film Cooling With Compound Angle Holes: Adiabatic Effectiveness

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1. Comparison of Showerhead Film Cooling and Double Wall Cooling in a Guide Vane Leading Edge with Hot Streak;International Journal of Gas Turbine, Propulsion and Power Systems;2024

2. Assessment of a virtual boundary concept for efficient modeling of turbine film cooling;Numerical Heat Transfer, Part A: Applications;2023-12-29

3. Numerical study of discrete film cooling near the rudder shaft of a hypersonic air fin model;Numerical Heat Transfer, Part A: Applications;2023-04-03

4. A Numerical Investigation of Heat Transfer Characteristics with Varying Film Cooling Hole Shapes for Gas Turbine Blade Cooling;Journal of the Korean Society for Precision Engineering;2022-06-01

5. Film cooling performance for the cratered film-cooling holes with various coolant crossflow orientations;Numerical Heat Transfer, Part A: Applications;2021-09-27

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