Abstract
The aim of this paper was to presents a identification of dynamic behavior and response analysis of a glass-epoxy plate. The numerical simulation were carried out on model plate made of glass-epoxy, and the corresponding frequency response functions have been calculate. An initial study into the dynamic loads of this method has been considered, the use of the finite element method makes it possible to develop the model of the plate, the model is used to evaluate the maximal (displacement, strain and stress) and the natural frequencies, mode shapes of plate in composite glass-epoxy under damage condition.
The stress should be increased to improve the strength of the plate. The experimental results can provide a reference for analysts and designers of composite material in aeronautical systems.
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Chellil, A., Lecheb, S., Mechakra, H., Chellil, S., Safi, B. (2018). Experimental and Numerical Damaged Characteristics in Composite Plate with Crack Growth by Vibration Analysis. In: Abdelbaki, B., Safi, B., Saidi, M. (eds) Proceedings of the Third International Symposium on Materials and Sustainable Development. SMSD 2017. Springer, Cham. https://doi.org/10.1007/978-3-319-89707-3_31
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DOI: https://doi.org/10.1007/978-3-319-89707-3_31
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