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- W2138820171 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." @default.
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- W2138820171 date "2013-01-01" @default.
- W2138820171 modified "2023-10-17" @default.
- W2138820171 title "Behavior of Single-Lap Bolted Joint Subjected to Dynamic Transverse Load" @default.
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- W2138820171 doi "https://doi.org/10.1007/978-3-642-37143-1_21" @default.
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