Unsteady effects in a thin viscous shock layer near a threedimensional stagnation point of a body moving with given acceleration and deceleration

DOI10.1007/BF01090354zbMath0476.76063OpenAlexW2055229403MaRDI QIDQ1160047

S. H. Smith

Publication date: 1981

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

Full work available at URL: https://doi.org/10.1007/bf01090354

zbMATH Keywords

inviscid partreflection coefficientslipaxisymmetricviscous sublayerRankine-Hugoniot relationsspherical coordinate systemthin shock layertemperature discontinuitycoefficient of thermal accomodationcompletely viscous layerratio of specific heats and Reynolds numberunsteady flow near stagnation point

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20) Hypersonic flows (76K05) Euler-Poisson-Darboux equations (35Q05)

Related Items (2)

Viscous shock layer near the stagnation point on a rotating body with unsteady injection and surface cooling ⋮ Flow regimes of a viscous gas in a thin three-dimensional shock layer near a surface with small curvatures

Cites Work

• Unnamed Item
• Unsteady heat transfer on boundary layer growth at the forward stagnation point
• An Interesting Result on Almost Square Matrices and the Cauchy-Binet Theorem
• Unsteady Laminar Boundary Layers
• Unsteady laminar compressible boundary-layer flow at a three-dimensional stagnation point
• Asymptotic solutions of the energy equation for viscous supersonic flow past corners
• Local similarity expansions of the boundary- layer equations

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