The unsteady boundary layer flow in a convergent channel

Abstract

An incompressible fluid is at rest in a converging channel between intersecting planes when, at some moment of time, the flow towards a sink at the point of intersection is set up impulsively. The motion is taken to be of the boundary layer type, and it is found that the transient part of the flow decays algebraically as the steady state motion becomes dominant. The final decay takes place at the edge of the boundary layer, with the viscous forces affecting the unsteady flow in a region that eventually lies outside the steady state boundary layer.