Fig. 21From: Multiscale analysis of complex aeronautical structures using robust non-intrusive couplingLarge scale effect of the local cut. Comparison between the submodeling and the iterative non-intrusive approaches: distribution of the difference between the two global horizontal displacements (mm): \(U_{\mathrm {non\text {-}intrusive}}-U_{\mathrm {submodeling}}\) (floor, stiffeners and frames not represented)Back to article page