Fig. 4From: Multiscale analysis of complex aeronautical structures using robust non-intrusive couplingIllustration of the proposed pragmatic strategy based on a transition mesh generation. Starting from a the initial meshes, step b: determination of the patch (grey area) and a new interface (red line) and step c transition mesh generation making appear two distinct interfaces (red line: global/local, blue line: shell/solid)Back to article page