Hypersonic boundary-layer separation on a cold wall

DOI10.1017/S0022112094002089zbMath0837.76019MaRDI QIDQ4319588

J. D. A. Walker, Ruslan M. Kerimbekov, Anatoly I. Ruban

Publication date: 19 May 1996

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

zbMATH Keywords

singularitydisplacement thicknessasymptotic theorytriple-deck theoryinviscid-inviscid interaction

Mathematics Subject Classification ID

Related Items (8)

Global stability of supersonic flow over a hollow cylinder/flare ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ The influence of wall cooling on hypersonic boundary-layer separation and stability ⋮ Separation phenomenon in a hypersonic flow with strong wall cooling: Subcritical regime ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow ⋮ Marginal separation in three-dimensional flows ⋮ 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
• On an Integral Equation of Marginal Separation
• Boundary-Layer Interaction Theory
• Marginal Separation
• D’Alembert’s Paradox
• Solutions of the Navier–Stokes Equation at Large Reynolds Number
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Incompressible Laminar Boundary Layers on a Parabola at Angle of Attack: A Study of the Separation Point

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