Heat transfer in a trailing cooling channel using ejection slot with different chordwise length ratio of impingement cavity-Reference-Cited by-同舟云学术

Heat transfer in a trailing cooling channel using ejection slot with different chordwise length ratio of impingement cavity

Published:2021-11-25 Issue: Volume: Page:1-18
ISSN:0891-6152
Container-title:Experimental Heat Transfer
language:en
Short-container-title:Experimental Heat Transfer

Author:

Deng Hongwu¹,Wu Jiangxue²,Zhu Jianqin¹,Tao Zhi¹,Tian Shuqing³

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-engine Aero-thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing, China

2. BeiJing Aerospace Propulsion Institute, Beijing, China

3. R&d Center Dept of Discipline Engineering, Avic Commercial Aircraft Engine Co., Ltd, Shanghai, China

Publisher

Informa UK Limited

Subject

Electrical and Electronic Engineering,Instrumentation,Control and Systems Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/08916152.2021.1977426

Reference20 articles.

1. Heat Transfer Between Blockages With Holes in a Rectangular Channel

2. Combined Effects of Perforated Blockages and Pin Fins in a Trailing Edge Internal Cooling Duct

3. Trailing edge cooling of a gas turbine blade with perforated blockages with inclined holes

4. Heat Transfer and Pressure Drop in Pin-Fin Trapezoidal Ducts

5. Lateral-Flow Effect on Endwall Heat Transfer and Pressure Drop in a Pin-Fin Trapezoidal Duct of Various Pin Shapes

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