A comparison of the models of a thin and a complete viscous shock layer in the problem of the supersonic flow of a viscous gas past blunt cones

DOI10.1016/0021-8928(89)90083-XzbMath0734.76034OpenAlexW2991653849MaRDI QIDQ811248

G. A. Tirskij, Sergey V. Utyuzhnikov

Publication date: 1989

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(89)90083-x

zbMATH Keywords

asymptotic approachshock wavespherically blunted conesthin (hypersonic) viscous shock layerviscous heat conducting supersonic gas

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items

Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers ⋮ Viscous shock layer on a plate in hypersonic flow ⋮ Comparison of gas-dynamic models for hypersonic flow past bodies

Cites Work

• Unnamed Item
• Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip
• Non-Navier Stokes viscous flow computations
• Numerical Solutions of Hypersonic Viscous Shock-Layer Equations
• Computation of viscous gas flow with high Reynolds number past a blunt body
• Local similarity expansions of the boundary- layer equations
• Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies