I. Introduction
The aim of our study is to model complex parts of large turbo-generators. The resort to indirect coupling [12], [3] allows the use of numerically adapted meshes for each subproblem. It also avoids to take into account irrelevant parts of some problems (e.g., air domain for mechanical study) while facilitating the remeshing process. Such data transfers allow the replacement of subcodes or subproblems and are the most difficult stage of the method [1], [6].