The effect of Mach number on unstable disturbances in shock/boundary-layer interactions
Yao, Y., Krishnan, L., Sandham, N. and Roberts, G.
The effect of Mach number on unstable disturbances in shock/boundary-layer interactions.
Physics of Fluids, 19 (5).
Available from: http://eprints.uwe.ac.uk/17712
Full text not available from this repository
Publisher's URL: http://dx.doi.org/10.1063/1.2720831
|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|
|Deposited On:||16 Oct 2012 14:31|
|Last Modified:||15 Nov 2016 22:54|
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