Analysis and Optimization of Double-Jet Film-Cooling Holes-Reference-Cited by-同舟云学术

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Analysis and Optimization of Double-Jet Film-Cooling Holes

Published:2013-04 Issue:2 Volume:27 Page:246-254
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Choi Dae-Woong¹,Lee Ki-Don¹,Kim Kwang-Yong¹

Affiliation:

1. Department of Mechanical Engineering, Inha University, Incheon 402-751, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.T4060

Reference26 articles.

1. A Detailed Analysis of Film-Cooling Physics: Part I—Streamwise Injection With Cylindrical Holes

2. Effect of compound angle injection on flat surface film cooling with large streamwise injection angle

3. Film Cooling Effectiveness Downstream of Compound and Fan-Shaped Holes

4. Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes

5. Film cooling effectiveness from trenched shaped and compound holes

Cited by 24 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. A study of vortex generator effects on fan-shaped hole cooling performance;International Journal of Thermal Sciences;2024-06

2. Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design;Journal of Turbomachinery;2023-12-14

3. Aircraft engine nozzle guide vane surface temperature optimization;Heliyon;2023-09

4. Transpiration cooling of high pressure turbine vane with optimized porosity distribution;Applied Thermal Engineering;2023-03

5. Numerical Study of Double-Jet Film Cooling on a Semi-Cylindrical Leading Edge;Journal of Thermal Science and Engineering Applications;2022-06-24

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