Correlation between density and temperature fluctuations of hypersonic turbulent boundary layers at Ma∞ = 8-Reference-Cited by-同舟云学术

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Correlation between density and temperature fluctuations of hypersonic turbulent boundary layers at Ma∞ = 8

Published:2020-07-01 Issue:7 Volume:10 Page:075101
ISSN:2158-3226
Container-title:AIP Advances
language:en
Short-container-title:AIP Advances

Author:

Li Xin¹²,Tong Fu-Lin¹³,Yu Chang-Ping¹^ORCID,Li Xin-Liang¹²^ORCID

Affiliation:

1. LHD, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China

2. School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China

3. Computational Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang 621000, China

Funder

National Numerical Wind Tunnel Project

The National Key Research and Development Program of China

Strategic Priority Research Program of Chinese Academy of Sciences

Science Challenge Project

NSFC Projects

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0013299

Reference27 articles.

1. Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction

2. Near-wall dynamics of compressible boundary layers

3. A numerical study of compressible turbulent boundary layers

4. Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number

5. Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Compressibility effect in compressible turbulent channel flows;SCIENTIA SINICA Physica, Mechanica & Astronomica;2023-03-20

2. On the drag reduction mechanism of hypersonic turbulent boundary layers subject to heated wall blowing;Advances in Aerodynamics;2023-02-21

3. Properties of the compressibility and transport motion in wall-bounded turbulent flows at Mach 8;International Journal of Modern Physics C;2022-01-06

4. Direct numerical simulations of a supersonic turbulent boundary layer subject to velocity-temperature coupled control;Physical Review Fluids;2021-04-06

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