Numerical Studies on Heat Transfer of Supersonic Combustion-Gas Jet Impingement on Perpendicular Flat Plate-Reference-Cited by-同舟云学术

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Numerical Studies on Heat Transfer of Supersonic Combustion-Gas Jet Impingement on Perpendicular Flat Plate

Published:2021-04-09 Issue: Volume: Page:1-17
ISSN:0145-7632
Container-title:Heat Transfer Engineering
language:en
Short-container-title:Heat Transfer Engineering

Author:

Tian Yuyan¹,Li Wenhao²,Xue Pu²,Gao Zhenxun¹³

Affiliation:

1. School of Aeronautic Science and Engineering, Beihang University, Beijing, China

2. Beijing Institute of Space Long March Vehicle, Beijing, China

3. Laboratory of Aero-thermal Protection Technology for Aerospace Vehicles, China Aerospace Science and Technology Corporation, Beijing, China

Funder

National Numerical Wind

Publisher

Informa UK Limited

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Link

https://www.tandfonline.com/doi/pdf/10.1080/01457632.2021.1906518

Reference40 articles.

1. The near wall jet of a normally impinging, uniform, axisymmetric, supersonic jet

2. A Dynamics Study for the Hot Stage Separation of a Multistage Rocket with a Coupled CFD Flight Mechanics Approach

3. Multibody Dynamic Simulator for Launch Vehicles Stage Separation Studies

4. Influence of shock structure on heat transfer characteristics in supersonic under-expanded impinging jets

5. An experimental study of the oscillatory flow structure of tone-producing supersonic impinging jets

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