Film cooling performance under plasma aerodynamic actuation and spoiler ribs of an internal cooling channel based on Suzen model-Reference-Cited by-同舟云学术

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Film cooling performance under plasma aerodynamic actuation and spoiler ribs of an internal cooling channel based on Suzen model

Published:2024-03-18 Issue: Volume: Page:1-21
ISSN:1040-7782
Container-title:Numerical Heat Transfer, Part A: Applications
language:en
Short-container-title:Numerical Heat Transfer, Part A: Applications

Author:

Sun Jie¹,Xie Gongnan¹,Sunden Bengt²^ORCID,Wang Jin³

Affiliation:

1. School of Marine Science and Technology, Northwestern Polytechnical University, Xi’an, China

2. Professor Emeritus of Lund University, BS Heat Transfer and Fluid Flow, Angelholm, Sweden

3. School of Energy and Environmental Engineering, Hebei University of Technology, Tianjin, China

Funder

National Natural Science Foundation of China

National 111 Project

Natural Science Foundation of Hebei Province of China

Special Project of Science and Technology Winter Olympics in the Hebei Technology Innovation Guidance Plan

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/10407782.2024.2328879

Reference29 articles.

1. Effect of coolant pulsation on film cooling performance on turbine vane

2. Film cooling performance for the cratered film-cooling holes with various coolant crossflow orientations

3. Creep detection of Hastelloy X material for gas turbine components with nonlinear ultrasonic frequency modulation

4. Particle deposition patterns on high-pressure turbine vanes with aggressive inlet swirl

5. Effects of plasma actuation and hole configuration on film cooling performance

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