Numéro |
J. Phys. IV France
Volume 134, August 2006
EURODYMAT 2006 - 8th International Conference on Mechanical and Physical Behaviour of Materials under Dynamic Loading
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Page(s) | 507 - 514 | |
DOI | https://doi.org/10.1051/jp4:2006134078 | |
Publié en ligne | 26 juillet 2006 |
J. Cirne, R. Dormeval, et al.
J. Phys. IV France 134 (2006) 507-514
DOI: 10.1051/jp4:2006134078
Elastic wave propagation in hexagonal honeycomb sandwich panels: Physical understanding and numerical modeling
A. Grédé, B. Tie and D. AubryLaboratoire de Mécanique Sols-Structures-Matériaux (CNRS UMR 8579), École Centrale Paris, Grande Voie des Vignes, 92295 Châtenay Malabry Cedex, France
Published online: 26 July 2006
Abstract
This paper gives theoretical and numerical analyses of
elastic wave propagation phenomena in sandwich panels with a honeycomb core,
especially when the frequency domain of interest is large and involves high
frequencies. In the literature, computational models represent rather these
panels as an equivalent homogeneous continuum using shell type finite
element mesh than use a detailed “geometrically exact” finite element
mesh. The reliability of such homogenized models is critically dependent
upon the pertinence of the homogeneous constitutive model and the shell
kinematics, as far as the shortest wavelength to consider is smaller than
the size of honeycomb cells and than the shell thickness. Herein, it is
proposed to discus this issue and to qualify the classical homogeneous
models and one- or multi-layered shell kinematical models with respect to
the frequency domain of interest. The quality assessment is made by
comparison with both numerical simulations of a small detailed geometrically
exact finite element model and experimental results on a large sandwich
plate. Several criteria of qualification in terms of energy and/or
displacement are considered.
© EDP Sciences 2006