Investigation of stationary flow of viscous gas in a thin three- dimensional shock layer

DOI10.1007/BF01089647zbMath0461.76053MaRDI QIDQ1152775

S. H. Smith

Publication date: 1980

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

zbMATH Keywords

stagnation pointthree-dimensionalshock layerblunt surfacesweptback wing

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Asymptotic approximations, asymptotic expansions (steepest descent, etc.) (41A60) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (5)

Analytic investigation of friction and heat transfer in the neighborhood of a three-dimensional stagnation point at low and moderate Reynolds numbers ⋮ Unsteady viscous shock layer near the leading edge of a wing of infinite span ⋮ Three-dimensional thin viscous shock layer in the absence of planes of symmetry in the flow ⋮ 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 ⋮ Flow regimes of a viscous gas in a thin three-dimensional shock layer near a surface with small curvatures

Cites Work

• Unnamed Item
• On hypersonic flows of viscous heat-conducting gases
• Local similarity expansions of the boundary- layer equations

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