Two-dimensional numerical investigations of small-amplitude disturbances in a boundary layer at Ma=4.8: Compression corner versus impinging shock wave
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Publication:3554476
DOI10.1063/1.1738414zbMath1186.76409OpenAlexW2072699945MaRDI QIDQ3554476
Andreas Babucke, Ulrich Rist, Alessandro Pagella
Publication date: 22 April 2010
Published in: Physics of Fluids (Search for Journal in Brave)
Full work available at URL: https://semanticscholar.org/paper/fa525932ec146fae6f17ebd5682e2dd0d5ea54df
Related Items (6)
ON THE RESPONSE OF SHOCK-INDUCED SEPARATION BUBBLE TO SMALL AMPLITUDE DISTURBANCES ⋮ Sidewall effects in laminar ramp induced shockwave boundary layer interactions ⋮ Instability and low-frequency unsteadiness in a shock-induced laminar separation bubble ⋮ Analysis of the two-dimensional dynamics of a Mach 1.6 shock wave/transitional boundary layer interaction using a RANS based resolvent approach ⋮ The effect of Mach number on unstable disturbances in shock/boundary-layer interactions ⋮ Disturbance evolution in a Mach 4.8 boundary layer with two-dimensional roughness-induced separation and shock
Cites Work
- Compact finite difference schemes with spectral-like resolution
- Spatial numerical simulations of linear and weakly nonlinear wave instabilities in supersonic boundary layers
- Numerical investigations of small-amplitude disturbances in a boundary layer with impinging shock wave at Ma=4.8
- Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685
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