Wedge-induced turbulent boundary-layer separation on a roughened surface at Mach 6.0-Reference-Cited by-同舟云学术

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Wedge-induced turbulent boundary-layer separation on a roughened surface at Mach 6.0

Published:1991-11 Issue:6 Volume:28 Page:636-645
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Disimile P. J.¹,Scaggs N. E.²

Affiliation:

1. University of Cincinnati, Cincinnati, Ohio 45221

2. Air Force Wright Research and Development Center, Wright-Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.26293

Reference20 articles.

1. Golden, M. S. "A Review of Aerothermal Problems Associated with Hypersonic Flight," AIAA Paper 86-0267, Jan.1986.

Cited by 3 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. Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall;Chinese Journal of Aeronautics;2021-05

2. Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall;NEUROPSYCH DIS TREAT;2021

3. Effect of Surface Roughness on Unseparated Shock-Wave/Turbulent Boundary-Layer Interactions;AIAA Journal;2002-08

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