Nonsimilar boundary layers on the leeside of cones at incidence

DOI10.1016/0045-7930(83)90029-4zbMath0511.76027OpenAlexW2069002527MaRDI QIDQ1839125

Keith Stewartson, Tuncer Cebeci, Susan N. Brown

Publication date: 1983

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(83)90029-4

zbMATH Keywords

boundary layers growingexternal Mach number and enthalpy ratioincidence parameter of Mooresimilarity equations for leeward line of symmetry of conesingularity of type Stewartson and Simpson for entry flow in curved pipewindward line of symmetrywindward to leeward integrations

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05)

Related Items (4)

Marginal separation of a three-dimensional boundary layer on a line of symmetry ⋮ Singularities in the boundary layer on a cone at incidence ⋮ Singularity in the solution of the equations of a three-dimensional boundary layer due to the collision of wall jets ⋮ A study of wing-fuselage interaction

Cites Work

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• ON A SINGULARITY INITIATING A BOUNDARY-LAYER COLLISION
• Symmetry Plane Viscous Layer on a Sharp Cone
• Laminar boundary layer on a cone near a plane of symmetry.
• Viscous flow past a flat plate with uniform injection
• Supersonic laminar boundary layer near the plane of symmetry of a cone at incidence
• The solution of sharp-cone boundary-layer equations in the plane of symmetry
• ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION

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