The paper describes a local solution method for the calculation of the
interaction between a weak shock front and a turbulent boundary layer
on a swept wing. A multiple-deck approach allows the simplification o
f the governing equations according to the physical character of each
deck. The mathematical model is based upon small-perturbation theory.
The final boundary-layer solution is given by an iterative coupling of
the solutions for each domain. The results are compared with experime
nts and with other theoretical solutions.