Nonsimilar boundary layers on the leeside of cones at incidence

Author:

Cebeci Tuncer,Stewartson Keith,Brown S.N.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference17 articles.

1. Three-dimensional compressible laminar boundary-layer flow;Moore;NACA Tech. Note No. 2279,1951

2. Laminar boundary layer on cone in supersonic flow at large angle of attack;Moore;NACA Rept. No. 1132,1953

3. The shock layer concept and three-dimensional hypersonic boundary layers;Cheng;Cornell Aero. Lab. Rept. AF-1285-A-3,1961

4. Supersonic laminar boundary layer near the plane of symmetry of a cone at incidence;Roux;J. Fluid Mech.,1972

5. The solution of sharp-cone boundary-layer equations in the plane of symmetry;Murdock;J. Fluid Mech.,1972

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1. Singularities of the boundary layer equations and the structure of the flow in the vicinity of the convergence plane on conical bodies;Fluid Dynamics;2007-08

2. Compressible Boundary-Layer Theory;Analytical Fluid Dynamics, Second Edition;2000-12-21

3. Interacting Laminar and Turbulent Boundary Layers;Recent Advances in Boundary Layer Theory;1998

4. Singularities encountered in three-dimensional boundary layers under an adverse or favourable pressure gradient;Philosophical Transactions of the Royal Society of London. Series A: Physical and Engineering Sciences;1995-07-15

5. Singularities in the boundary layer on a cone at incidence;Fluid Dynamics;1994

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