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

Yao, Yufeng; Krishnan, L.; Sandham, N.D.; Roberts, G.

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering

L. Krishnan

N.D. Sandham

G. Roberts

Journal Article Type	Article
Publication Date	May 1, 2007
Journal	Physics of Fluids
Print ISSN	1070-6631
Publisher	AIP Publishing
Peer Reviewed	Peer Reviewed
Volume	19
Issue	5
DOI	https://doi.org/10.1063/1.2720831
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
Public URL	https://uwe-repository.worktribe.com/output/1028392
Publisher URL	http://dx.doi.org/10.1063/1.2720831