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The solution of sharp-cone boundary-layer equations in the plane of symmetry

Published online by Cambridge University Press:  29 March 2006

John W. Murdock
Affiliation:
The Aerospace Corporation, San Bernardino, California

Abstract

A detailed study has been made of the solutions to cone boundary-layer equations in the symmetry plane in order to increase understanding of the mathematical nature and physical meaning of these solutions. A typical set of symmetry-plane solutions is presented. Included in this set are various solution branches not previously published. A double-valued solution curve is found which has not been studied prior to this time except at one trivial point. The extension of an existing solution branch through a removable singular point has also been accomplished. The solutions presented are categorized according to whether they are dependent on or independent of the boundary layer outside the symmetry plane. The region in which no solutions to the usual symmetry-plane equations exist is examined. Solutions in which the usual boundary-layer model predicts that conservation of mass is not satisfied at the symmetry plane are discussed. Non-analytical behaviour at the symmetry plane is also investigated. In both of these cases a boundary region exists at the symmetry plane.

Type
Research Article
Copyright
© 1972 Cambridge University Press

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References

Boericke, R. R. 1969 The laminar boundary layer on a cone at incidence in supersonic flow. Ph.D. thesis, Polytechnic Institute of Brooklyn. (See also 1970 A.I.A.A. 8th Aerospace Sciences Meeting Paper, 70–48.)
Cheng, H. K. 1961 The shock layer concept and three-dimensional hypersonic boundary layers. Cornell Aero. Lab. Rep. AF-1285-A-3.Google Scholar
Dwyer, H. A. 1971 Boundary layer on a hypersonic sharp cone at small angle of attack A.I.A.A. J. 9, 277284.Google Scholar
Ferri, A. 1950 Supersonic flow around circular cones at angles of attack. N.C.A. Tech. Note. no. 2236.Google Scholar
Libby, P. A. 1967 Heat and mass transfer at a general three-dimensional stagnation point A.I.A.A. J. 5, 507517.Google Scholar
Libby, P. A. & Liu, T. M. 1968 Some similar laminar flows obtained by quasi-linearization A.I.A.A. J. 6, 15411548.Google Scholar
Moore, F. K. 1951 Three-dimensional compressible laminar boundary-layer flow. N.A.C.A. Tech. Note, no. 2279.Google Scholar
Moore, F. K. 1953 Laminar boundary layer on cone in supersonic flow at large angle of attack. N.A.C.A. Rep. no. 1132. (See also 1952 N.A.C.A. Tech. Note, no. 2844.)Google Scholar
Moore, F. K. 1956 Three-dimensional boundary layer theory Advances In Applied Mechancis, 4, 159228.Google Scholar
Reshotko, E. 1957 Laminar boundary layer with heat transfer on a cone at angle of attack in a supersonic stream. N.A.C.A. Tech. Note, no. 4152.Google Scholar
Roux, B. 1972 Supersonic laminar boundary layer near the plane of symmetry of a cone at incidence J. Fluid Mech. 51, 114.Google Scholar
Rubin, S. G. 1966 Incompressible flow along a corner J. Fluid Mech. 26, 97110.Google Scholar
Stewartson, K. 1961 Viscous flow past a quarter-infinite plate J. Aerospace Sci. 28, 110.Google Scholar
Trella, M. & Libby, P. A. 1965 Similar solutions for the hypersonic boundary layer near a plane of symmetry A.I.A.A. J. 3, 7583.Google Scholar
Van Dyke, M. 1964 Perturbation Methods in Fluid Mechanics. Academic.
Van Dyke, M. 1969 Higher-order boundary layer theory Ann. Rev. Fluid Mech. 1, 265292.Google Scholar
Vvedenskaya, N. D. 1966 Calculation of the boundary layer arising in a flow about a cone under an angle of attack Zh. vychisl. Mat. mat. Fizl. 6, 304312.Google Scholar
Wang, K. C. 1971 On the determination of the zones of influence and dependence for three-dimensional boundary-layer equations J. Fluid Mech. 48, 397404.Google Scholar