Abstract
The “Centre d’Etudes de Gramat (C.E.G.)” is working on the modelling of the behaviour of double walled aeronautical structures submitted to impulsive loading. These structures are made of a composite lining panel, on which the pressure loads apply, and an aluminum alloy skin. The lining panel and the skin are both attached on frames which separate them (figure 1).
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© 1998 Springer Science+Business Media Dordrecht
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Moreno, A. (1998). Dynamic Behaviour of Sandwich Structures Used in Air Transport. In: Vautrin, A. (eds) Mechanics of Sandwich Structures. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-9091-4_24
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DOI: https://doi.org/10.1007/978-94-015-9091-4_24
Publisher Name: Springer, Dordrecht
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