Development and separation of a compressible laminar boundary layer under the action of a very sharp adverse pressure gradiant

DOI10.1017/S0022112078000233zbMath0371.76059MaRDI QIDQ4147722

Samuel Newby Curle

Publication date: 1978

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (4)

Boundary layer separation for the steady compressible Prandtl equation ⋮ Some aspects related to the asymptotic solutions of the laminar boundary- layer equations with heat flux ⋮ Effects of a sharp pressure rise on a compressible laminar boundary layer, when the Prandtl number is σ = 0.72 ⋮ On a class of compressible laminar boundary-layer flows and the solution behaviour near separation

Cites Work

• 9.—Development and Separation of a Laminar Boundary Layer, under the Action of a Very Sharp Constant Adverse Pressure Gradient
• Steady flow in the laminar boundary layer of a gas
• Correlated incompressible and compressible boundary layers

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