Finite Element Analysis (FEA) of Honeycomb Sandwich Panel for Continuum Properties Evaluation and Core Height Influence on the Dynamic Behavior
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics
2. Center of Excellence in Science and Applied Technologies
Abstract
Publisher
Trans Tech Publications, Ltd.
Subject
General Engineering
Link
https://www.scientific.net/AMR.326.1.pdf
Reference11 articles.
1. W. Burton, and A. Noor, Assessment of continuum models for sandwich panel honeycomb cores, Comput. Methods Appl. Mech. Eng., 145_3–4 (1997) 341–360.
2. L. Gibson, and M. Ashby, 1988. Cellular solids: Structure and properties, Pergamon, Oxford, U. K.
3. S. Kelsey, R. Gellatly, and B. Clark, The shear modulus of foil honeycomb cores. Aircr. Eng., 30(1958) 294–302.
4. F. Meraghni, F. Desrumaux, and M. Benzeggagh, Mechanical behavior of cellular core for structural sandwich panels. Composites, 30(1999), 767–779.
5. J. Penzien, and T. Diriksson, Effective shear modulus of honeycomb cellular structure. AIAA J., 2 (1964) 531–35.
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