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
Full text not available from this repository
Publisher's URL: http://dx.doi.org/10.1063/1.2720831
| Item Type: | Article |
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| 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 |
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| Faculty/Department: | Faculty of Environment and Technology
~Pre-2012 Faculty Structure > Faculty of Environment and Technology |
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| ID Code: | 17712 |
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| Deposited By: |
A. Clarke
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| Deposited On: | 16 Oct 2012 14:31 |
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| Last Modified: | 14 Mar 2013 14:46 |
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