Viscous shock layer near the stagnation point on a rotating body with unsteady injection and surface cooling

DOI10.1007/BF01051698zbMath0648.76050OpenAlexW2069717017MaRDI QIDQ1105450

S. H. Smith

Publication date: 1987

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

Full work available at URL: https://doi.org/10.1007/bf01051698

zbMATH Keywords

Euler equationsanalytic solutionstagnation pointboundary layer equationsstrong injectionviscous shock layerviscous shock layer equationsdivergent implicit scheme of the second order of approximationisolated bow shockNewtonian linearizationunsteady equationsUnsteady supersonic flow regimesvector sweep methods

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05)

Related Items (1)

Unsteady viscous shock layer near the leading edge of a wing of infinite span

Cites Work

• Unnamed Item
• 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
• Investigation of a class of swirling motions of dusty gas
• Flow regimes of a viscous gas in a thin three-dimensional shock layer near a surface with small curvatures
• Unsteady effects in a thin viscous shock layer near a threedimensional stagnation point of a body moving with given acceleration and deceleration
• Unsteady heat transfer on boundary layer growth at the forward stagnation point
• Unsteady laminar compressible boundary-layer flow at a three-dimensional stagnation point

This page was built for publication: Viscous shock layer near the stagnation point on a rotating body with unsteady injection and surface cooling