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MDA of Hexagonal Honeycomb Plates used for Space Applications

Authors: A. Boudjemai , M.H. Bouanane, Mankour, R. Amri, H. Salem, B. Chouchaoui


The purpose of this paper is to perform a multidisciplinary design and analysis (MDA) of honeycomb panels used in the satellites structural design. All the analysis is based on clamped-free boundary conditions. In the present work, detailed finite element models for honeycomb panels are developed and analysed. Experimental tests were carried out on a honeycomb specimen of which the goal is to compare the previous modal analysis made by the finite element method as well as the existing equivalent approaches. The obtained results show a good agreement between the finite element analysis, equivalent and tests results; the difference in the first two frequencies is less than 4% and less than 10% for the third frequency. The results of the equivalent model presented in this analysis are obtained with a good accuracy. Moreover, investigations carried out in this research relate to the honeycomb plate modal analysis under several aspects including the structural geometrical variation by studying the various influences of the dimension parameters on the modal frequency, the variation of core and skin material of the honeycomb. The various results obtained in this paper are promising and show that the geometry parameters and the type of material have an effect on the value of the honeycomb plate modal frequency.

Keywords: Satellite, honeycomb, finite element method, modal frequency, dynamic.

Digital Object Identifier (DOI):

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[1] Thimas P. Sarafin and Wiley J. Larson, spacecraft structures and mechanisms-from concept to launch, Microcosm, Inc. 1995.
[2] Wiley J. Larson and James R. Wertz, Space mission analysis and design, second edition, Microcosm, Inc. ISBN 0-7923-1998-2, 1992.
[3] Meifeng He, Wenbin Hu, A study on composite honeycomb sandwich panel structure, Materials and Design, 29 (2008) 709-713.
[4] A. Boudjemai, M. Bekhti, , M.H. Bouanane, A.M. Si Mohammed, G. Cooper and G. Richardson, Small satellite Computer-Aided Design and Manufacturing, pp.181-188, SP-581, August 2005, Proceedings of the European conference on Spacecraft Structures, Materials & Mechanical Testing, 10-12 May 2005, ISSN: 1609-042X
[5] A. Boudjemai, M.H. Bouanane and, M.A. Si Mohammed, Structural Modelling and Small Satellite Optimisation, page 51, Second International Congress Design and Modelling of Mechanical Systems, CMSM-07, proceeding, 12-21 march 2007, Monastir Tunisia.
[6] A. Boudjemai, M.H. Bouanane, L. Merad and M.A. Si Mohammed, Small Satellite Structural Optimisation Using Genetic Algorithm Approach, 3rd International Conference on Recent Advances in Space Technologies, RAST '07, pp. 398-406, Istanbul, Turkey, ISBN: 1-4244- 1057-6, ┬® IEEE 2007.
[7] Jeom Kee Paik, Anil K. Thayamballi, Gyu Sung Kim, The strength characteristics of aluminium honeycomb sandwich panels, Thin-Walled Structures 35 (1999) 205-231, ┬® Elsevier Science Ltd.
[8] Noor, A., Burton, W., and Bert, C. (1996), Computational models for sandwich panels and shells, Appl. Mech. Rev., 49(3), 155-199.
[9] Buannic N., Cartraud P., Quesnel T., (2003). Homogenization of corrugated core sandwich panels. Composite Structures, 59:299-312.
[10] XU Sheng-jin, Kong Xian-ren, Wang Ben-li, MA Xing-rui, Zhang Xiaochao, Method of equivalent analysis for statistics and dynamics behavior of orthotropic honeycomb sandwich plates, Acta Materiae Compositae Sinica; 2000, 17(3): 92-95.
[11] Fu M.H., Yin J.R., (1999). Equivalent elastic parameters of the honeycomb core. Acta Mechanica Sinica, 31:113-118.
[12] Hassani B., Hinton E., A review of homogenization and topology optimization II-analytical and numerical solution of homogenization equations. Computers and Structures, Vol.69, No.6, 1998, pp.719-738.
[13] XIA Li-juan, JIN Xian-ding, WANG Yang-bao. Equivalent analysis of honeycomb sandwich plates for satellite structure, Journal of Shanghai Jiao Tong University, 2003, 37(7): 999-1001.
[14] E. Roggero, M.Cerocchi, A.Rauschert, M. Sepulveda, A Analysis and design of a new alternative for satellite platforms, 10th Annual AIAA/USU Conference on Small Satellites, 1996.
[15] Burton, W.S., Noor, A.K. (1997), Assessment of continuum models for sandwich panel honeycomb cores, Computer Methods in Applied Mechanics and Engineering, 145(3-4), 341-360.
[16] S.D. Yu, W.L. Cleghorn, Free flexural vibration analysis of symmetric honeycomb panels, Journal of Sound and Vibration 284 (2005) 189- 204.
[17] P. Gri┼íkevi─ìius, D. Zeleniakiene, V. Lei┼íis, M. Ostrowski, Experimental and Numerical Study of Impact Energy Absorption of Safety Important Honeycomb Core Sandwich Structures, pp. 119-123, Materials Science (Medžiagotyra). Vol. 16, No. 2. 2010, ISSN 1392-1320.
[18] S. Debruyne , L. Mehrez, D. Vandepitte , E. Debrabandere , M. Hongerloot, The influence of design parameter variability on the dynamic behaviour of honeycomb sandwich panels, proceedings of isma2010 including usd2010, pp. 4875-4888.
[19] Kepeng QIU, Analysis and optimal design of lightweight sandwich structures and materials, PhD. Thesis, 2008.
[20] J Mackerle, Finite element analyses of sandwich structures: a bibliography (1980-2001), Engineering Computations, Vol.19, No.2, Mar 2002, pp.206-245.
[21] A. Anisetti, Non-linear Shunting of Piezo-actuators for Vibration Suppression, Master-s thesis, 2007.