Abstract
Bolted joints used in aeronautical structures are subject to vibrations, which can result in critical damage either from self-loosening or from fatigue. This study is devoted to the examination of the dynamic behavior of a simple bolted joint assembly subjected to quickly varying transverse load, which induces bending of the jointed plates. The adopted approach is based on finite element method, with a coupled bolt model and a penalty friction model, and implicit time simulation. Numerical result sets are presented and discussed.
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Ksentini, O., Combes, B., Abbes, M.S., Daidie, A., Haddar, M. (2013). Behavior of Single-Lap Bolted Joint Subjected to Dynamic Transverse Load. In: Haddar, M., Romdhane, L., Louati, J., Ben Amara, A. (eds) Design and Modeling of Mechanical Systems. Lecture Notes in Mechanical Engineering. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-37143-1_21
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DOI: https://doi.org/10.1007/978-3-642-37143-1_21
Publisher Name: Springer, Berlin, Heidelberg
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