9.—Development and Separation of a Laminar Boundary Layer, under the Action of a Very Sharp Constant Adverse Pressure Gradient

DOI10.1017/S0308210500016590zbMath0346.76030MaRDI QIDQ4116175

Samuel Newby Curle

Publication date: 1976

Published in: Proceedings of the Royal Society of Edinburgh: Section A Mathematics (Search for Journal in Brave)

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10)

Related Items (3)

Development of a laminar boundary layer under conditions of continuous incipient separation ⋮ Development and separation of a compressible laminar boundary layer under the action of a very sharp adverse pressure gradiant ⋮ Effects of a sharp pressure rise on a compressible laminar boundary layer, when the Prandtl number is σ = 0.72

Cites Work

• Unnamed Item
• Laminar boundary-layer flow near separation with and without suction
• ON GOLDSTEIN'S THEORY OF LAMINAR SEPARATION
• Trailing edge flows
• ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION

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