If a laminar two-dimensional viscous jet flows past a wall which is curved
up an adverse pressure gradient forms inside the jet owing to the streamlin
e curvature. As a consequence, solutions based on the boundary layer approx
imation may terminate in the form of a Goldstein-singularity or may develop
a marginal separation singularity. The fatter one is characterized by the
fact that the wall shear stress vanishes in a single point but immediately
recovers and can be used to develop a local interaction strategy which is a
ble to describe small separation regions. In the present study the results
obtained by Zametaev for locally plane walls are extended to include the ef
fects of two- and three-dimensional obstacles. Special emphasis is placed o
n the nonuniqueness of the solution for the wall shear stress distribution
which is governed by a nonlinear integro-differential equation.