Study on effects of inlet nonuniformities on aerothermal performance of NGV pressure side with different film cooling designs-Reference-Cited by-同舟云学术

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Study on effects of inlet nonuniformities on aerothermal performance of NGV pressure side with different film cooling designs

Published:2024-05-06 Issue: Volume: Page:1-22
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Wang Yi¹,Zhang Wenhao²,Li Ruocheng¹,Wang Zhiduo¹³,Wang Zhihao¹,Feng Zhenping¹

Affiliation:

1. Institute of Turbomachinery, School of Energy & Power Engineering, Xi’an Jiaotong University, P.R. China

2. AVIC Xi’an Aeronautics Computing Technique Research Institute, P.R. China

3. Aviation Engineering School, Air Force Engineering University, Xi’an, P.R. China

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/10407782.2024.2343032

Reference42 articles.

1. Advanced Cooling in Gas Turbines 2016 Max Jakob Memorial Award Paper

2. Redistribution of an inlet temperature distortion in an axial flow turbine stage

3. Recent advances in film cooling enhancement: A review

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