Separation phenomenon in a hypersonic flow with strong wall cooling: Subcritical regime

DOI10.1007/BF00417928zbMath0780.76022OpenAlexW2016438395MaRDI QIDQ687269

C. N. Zhikharev

Publication date: 20 December 1993

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00417928

zbMATH Keywords

hypersonic interaction parameterinteractive boundary-layer approachweak global interaction

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Hypersonic flows (76K05)

Related Items (2)

Hypersonic boundary-layer separation on a cold wall ⋮ The influence of wall cooling on hypersonic boundary-layer separation and stability

Cites Work

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• On an Integral Equation of Marginal Separation
• A reversed-flow singularity in interacting boundary layers
• D’Alembert’s Paradox
• On the High Reynolds Number Theory of Laminar Flows
• The interactive breakdown in supersonic ramp flow
• Hypersonic boundary-layer separation on a cold wall
• Self-induced separation
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Is the singularity at separation removable?
• ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION

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