DNS and analysis of a spatially evolving hypersonic turbulent boundary layer over a flat plate at Mach 8-Reference-Cited by-同舟云学术

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DNS and analysis of a spatially evolving hypersonic turbulent boundary layer over a flat plate at Mach 8

Published:2012-02-01 Issue:3 Volume:42 Page:282-293
ISSN:1674-7275
Container-title:SCIENTIA SINICA Physica, Mechanica & Astronomica
language:en
Short-container-title:Sci. Sin.-Phys. Mech. Astron.

Author:

LI XinLiang,MA YanWen,FU DeXun,LIANG Xian

Publisher

Science China Press., Co. Ltd.

Cited by 5 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. Effects of wall transpiration on the supersonic boundary-layer oblique-type transition;Journal of Physics: Conference Series;2024-05-01

2. Multiple-GPU accelerated high-order gas-kinetic scheme for direct numerical simulation of compressible turbulence;Journal of Computational Physics;2023-03

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 Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer;Communications in Computational Physics;2014-11-28

5. DNS of a spatially evolving hypersonic turbulent boundary layer at Mach 8;Science China Physics, Mechanics and Astronomy;2013-05-23

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