The objective of this work is to develop a modeling strategy for assemblies involving multiple joints in an aeronautical predesign context. In the process of designing large structures, industrial engineers usually get around computational limitations by using submodeling techniques. In order to take into account phenomena which vary during the global representation of the submodeling process, we propose a modeling approach for the scattering of these phenomena based on the Lack-Of-Knowledge (LOK) theory. The LOK model associated with a relevant deterministic joint model is updated based on experimental or simulated data. The proposed strategy is discussed and illustrated by the case of multiple-joint assemblies typical of those used in aeronautics.
