The influence of wall cooling on hypersonic boundary-layer separation and stability

DOI10.1017/S0022112096007690zbMath0890.76073MaRDI QIDQ4348873

J. D. A. Walker, Kevin W. Cassel, Anatoly I. Ruban

Publication date: 7 August 1997

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

compression ramphypersonic triple deck theory

Mathematics Subject Classification ID

Related Items (8)

A note on the appearance of wave-packets in steady-state triple-deck solutions of supersonic flow past a compression corner ⋮ Asymptotic theory of Mack-mode receptivity in hypersonic boundary layers due to interaction of a heating/cooling source and a freestream sound wave ⋮ Global stability of supersonic flow over a hollow cylinder/flare ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ Nonlinear interaction between a boundary layer and a liquid film ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow ⋮ Three-dimensionality of hypersonic laminar flow over a double cone ⋮ On wave-packets and discontinuities in triple-deck solutions of supersonic separated flows at a compression corner

Cites Work

• Separation phenomenon in a hypersonic flow with strong wall cooling: Subcritical regime
• Inviscid–viscous interaction on triple-deck scales in a hypersonic flow with strong wall cooling
• Marginal Separation
• On the stability and the numerical solution of the unsteady interactive boundary-layer equation
• Numerical solution of the local asymptotic problem of the unsteady separation of a laminar boundary layer in a supersonic flow
• Removal of Goldstein's singularity at separation, in flow past obstacles in wall layers
• The interactive breakdown in supersonic ramp flow
• Hypersonic boundary-layer separation on a cold wall
• An instability in supersonic boundary-layer flow over a compression ramp

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