On the theory of supersonic inviscid flow separation in gasdynamic problems

DOI10.1134/S0015462816050136zbMath1354.76086MaRDI QIDQ505950

R. Ya. Tugazakov

Publication date: 26 January 2017

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

Kelvin-Helmholtz instabilityshock wavesseparationself-similar conical flows

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Dimensional analysis and similarity applied to problems in fluid mechanics (76M55) Supersonic flows (76J20)

Related Items (2)

Nonlinear instability in the region of laminar-turbulent transition in supersonic three-dimensional flow over a flat plate ⋮ Boundary layer dynamics in a compressible gas. Numerical simulation

Cites Work

• Unnamed Item
• Conical gas flows with shock waves and turbulent boundary layer separation
• Theory of unsteady separation in supersonic flow around a convex corner
• Supersonic flow around a V-shaped wing at incidence and yaw
• Nonlinear conical flow of a gas

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