The effect of Mach number on unstable disturbances in shock/boundary-layer interactions

Yao, Y., Krishnan, L., Sandham, N.D. and Roberts, G. (2007) The effect of Mach number on unstable disturbances in shock/boundary-layer interactions. Physics of Fluids, 19(5), ISSN (print) 1070-6631

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Item Type: Article
Uncontrolled Keywords: Mach number, shock waves, flow instability, boundary layer turbulence, flow simulation, flow separation, bubbles, two-phase flow, white noise, convection, hypersonic flow, Navier-Stokes equations, shear turbulence, numerical analysis, small-amplitude disturbances, large-eddy simulation, impinging shock-wave, 3-dimensional boundary-layers, direct numerical-simulation, compression corner, transition prediction, stability, turbulence, flows
Research Area: General engineering and mineral and mining engineering
Faculty, School or Research Centre: Faculty of Engineering (until 2011) > Applied Engineering Research Centre (AERC)
Depositing User: William Downey
Date Deposited: 19 Jun 2007
Last Modified: 06 Feb 2012 15:30
URI: http://eprints.kingston.ac.uk/id/eprint/1319

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