Aerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic Flow-Reference-Cited by-同舟云学术

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Aerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic Flow

Published:2023-03 Issue:3 Volume:61 Page:1435-1439
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhou Bingkang¹,Yi Xiangyu²,Wang Zhaowei³,Li Zhufei¹

Affiliation:

1. University of Science and Technology of China, 230027 Hefei, People’s Republic of China

2. China Academy of Aerospace Aerodynamics, 100074 Beijing, People’s Republic of China

3. China Academy of Launch Vehicle Technology, 100076 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J062455

Reference36 articles.

1. CRITICAL HYPERSONIC AEROTHERMODYNAMIC PHENOMENA

2. Hypersonic Shock Wave Interactions on a V-Shaped Blunt Leading Edge

3. Hypersonic and High-Temperature Gas Dynamics, Second Edition

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