Flow regimes of a viscous gas in a thin three-dimensional shock layer near a surface with small curvatures

DOI10.1007/BF01091287zbMath0512.76063MaRDI QIDQ1050221

J. Blot

Publication date: 1982

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

zbMATH Keywords

asymptotic analysisthin layercoordinate system attachedinverse Reynolds and Mach numberspecific heat ratiothree-dimensional shock layer near fairly smooth body surfaceviscous regimes

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Shock waves and blast waves in fluid mechanics (76L05)

Related Items (4)

Viscous shock layer near the stagnation point on a rotating body with unsteady injection and surface cooling ⋮ Unsteady viscous shock layer near the leading edge of a wing of infinite span ⋮ Influence of rotation of the body and exterior vorticity on the heat transfer near the stagnation point of a blunt body in a supersonic stream ⋮ Numerical modeling of three-dimensional viscous flows using a space- marching method with pressure iterations

Cites Work

• Unnamed Item
• Investigation of stationary flow of viscous gas in a thin three- dimensional shock layer
• Unsteady effects in a thin viscous shock layer near a threedimensional stagnation point of a body moving with given acceleration and deceleration
• On hypersonic flows of viscous heat-conducting gases
• Local similarity expansions of the boundary- layer equations

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