Establishment of steady separated flow over a compression-corner in a free-piston shock tunnel-Reference-Cited by-同舟云学术

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Establishment of steady separated flow over a compression-corner in a free-piston shock tunnel

Published:1997-08-01 Issue:4 Volume:7 Page:249-253
ISSN:0938-1287
Container-title:Shock Waves
language:
Short-container-title:Shock Waves

Author:

Mallinson S.G.,Gai S.L.,Mudford N.R.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s001930050080.pdf

Cited by 15 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. Hypersonic shock impingement studies on a flat plate: flow separation of laminar boundary layers;Journal of Fluid Mechanics;2022-11-04

2. Wall temperature and bluntness effects on hypersonic laminar separation at a compression corner;Journal of Fluid Mechanics;2021-07-02

3. Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy;Journal of Fluid Mechanics;2020-12-07

4. Flow Characterization of a Hypersonic Expansion Tube Facility for Supersonic Combustion Studies;Journal of Propulsion and Power;2017-11

5. Establishment Times of Hypersonic Shock-Wave/Boundary-Layer Interactions in Intermittent Facilities;AIAA Journal;2017-09

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