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
Full text not available from this archive.
Official 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 |
| 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 |
Actions (Repository Editors)
 |
Item Control Page |