Direct numerical simulation of a supersonic turbulent boundary layer subject to adverse pressure gradient induced by external successive compression waves-Reference-Cited by-同舟云学术

Direct numerical simulation of a supersonic turbulent boundary layer subject to adverse pressure gradient induced by external successive compression waves

Published:2019-08 Issue:8 Volume:9 Page:085215
ISSN:2158-3226
Container-title:AIP Advances
language:en
Short-container-title:AIP Advances

Author:

Wang Xu¹,Wang Zhenguo¹^ORCID,Sun Mingbo¹,Wang Qiancheng¹^ORCID,Hu Zhiwei²^ORCID

Affiliation:

1. Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

2. Aerodynamics and Flight Mechanics, Faculty of Engineering and the Environment, University of Southampton, Southampton SO17 1BJ, UK

Funder

National Natural Science Foundation of China

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5112040

Reference68 articles.

1. Linear and nonlinear development of localized disturbances in zero and adverse pressure gradient boundary-layers

2. Streak instabilities in boundary layers beneath free-stream turbulence

3. On the scaling of turbulent separating boundary layers

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