The influence of grid overlapping on the convergence to a steady state
is studied for a time-dependent multidomain difference approximation
of a hyperbolic initial boundary value problem. Implicit dissipative d
ifference schemes for interior points and explicit matching conditions
at grid interfaces are considered. For a scalar model equation, it is
proved that when the total number of interior mesh points is large, t
he convergence speed is an increasing function of the overlapping leng
th. The convergence rate of the corresponding single domain treatment
is recovered for a sufficiently large overlapping length. For a partic
ular scheme, a quantitative analysis shows the existence of an optimal
overlapping length, equal to the CFL number, for which the multidomai
n scheme converges as well as and sometimes even better than the singl
e domain one in terms of the CPU time. Numerical experiments on a quas
i-one-dimensional supersonic flow in a duct show also that a proper ch
oice of the overlapping length ensures the same convergence rate as th
e one in the single domain calculation. Further applications to transo
nic flow calculations over single and two-element airfoils reveal the
good convergence property of the overlapping treatment even for proble
ms containing shocks.