Shock/shock and shock/boundary layer interactions in an axisymmetric steady laminar flow
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-003-0187-0.pdf
Cited by 8 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. A conjugate axisymmetric model of a high-pressure shock-tube facility;International Journal of Numerical Methods for Heat & Fluid Flow;2014-04-29
2. H2 injection and combustion in a Mach 5 air inlet through a Viscous Mach Interaction;European Journal of Mechanics - B/Fluids;2010-09
3. Shock wave-induced extremely high temporal and spatial oscillating pressure peaks;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2008-05-01
4. Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows;Shock Waves;2008-04-18
5. Richtmyer-Meshkov instability induced by shock-bubble interaction: Numerical and analytical studies with experimental validation;Physics of Fluids;2006-03
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