Multi-optimization of a specific laminated cooling structure for overall cooling effectiveness and pressure drop-Reference-Cited by-同舟云学术

Multi-optimization of a specific laminated cooling structure for overall cooling effectiveness and pressure drop

Published:2020-10-28 Issue:3 Volume:79 Page:195-221
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Wang Chen¹,Zhang Jingzhou¹,Wang Chunhua¹,Tan Xiaoming¹

Affiliation:

1. Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, School of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, P.R. China

Funder

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

Condensed Matter Physics,Numerical Analysis

Link

https://www.tandfonline.com/doi/pdf/10.1080/10407782.2020.1835105

Reference51 articles.

1. Gas Turbine Heat Transfer: Ten Remaining Hot Gas Path Challenges

2. Recent Studies in Turbine Blade Internal Cooling

3. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines

4. Recent Advances of Internal Cooling Techniques for Gas Turbine Airfoils

5. Thermo-fluid-dynamics of submerged jets impinging at short nozzle-to-plate distance: A review

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