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

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

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Publisher's URL: http://dx.doi.org/10.1063/1.2720831


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
Faculty/Department:Faculty of Environment and Technology
ID Code:17712
Deposited By: A. Clarke
Deposited On:16 Oct 2012 14:31
Last Modified:12 Aug 2013 08:08

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