A Finite Difference Method for Solving the Laminar Boundary Layer Equations Near a Wake Neck

A Finite Difference Method for Solving the Laminar Boundary Layer Equations Near a Wake Neck
Author: Eric Baum
Publisher:
Total Pages: 22
Release: 1965
Genre:
ISBN:

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A laminar wake model is studied which assumes that the boundary layer equations are valid in a shear layer on the axis of symmetry, and that the local pressure is determined by a displacement interaction with the inviscid outer flow. The finite difference method used places no restrictions on the shape of the velocity profile. The qualitative features of the solution are the same as those found by previous investigators using integral methods, in that an otherwise arbitrary initial condition (the local free stream Mach number) is determined by the fact that only a particular value results in a physically meaningful solution. Two methods of finding the particular solution are investigated. (Author).

Inverse Solutions for Laminar Boundary-layer Flows with Separation and Reattachment

Inverse Solutions for Laminar Boundary-layer Flows with Separation and Reattachment
Author: James Edward Carter
Publisher:
Total Pages: 72
Release: 1975
Genre: Boundary layer
ISBN:

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Numerical solutions of the laminar, incompressible boundary-layer equations are presented for flows involving separation and reattachment. Regular solutions are obtained with an inverse approach in which either the displacement thickness or the skin friction is specified; the pressure is deduced from the solution. A vorticity--stream-function formulation of the boundary-layer equations is used to eliminate the unknown pressure. Solutions of the resulting finite-difference equations, in which the flow direction is taken into account, are obtained by several global iteration schemes which are stable and have unconditional diagonal dominance. Results are compared with Klineberg and Steger's separated boundary-layer calculations, and with Briley's solution of the Navier-Stokes equations for a separated region. In addition, an approximate technique is presented in which the streamwise convection of vorticity is set equal to zero in the reversed flow region; such a technique results in a quick forward-marching procedure for separated flows.