Articles | Volume 11, issue 2
https://doi.org/10.5194/ms-11-317-2020
https://doi.org/10.5194/ms-11-317-2020
Research article
 | 
11 Sep 2020
Research article |  | 11 Sep 2020

Comparative study of dynamically equivalent modeling methods for honeycomb sandwich structure: numerical simulations and experiments

Ning Guo, Hao Chen, Zhong Zhang, Fei Du, and Chao Xu

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Subject: Structural Mechanics | Techniques and Approaches: Numerical Modeling and Analysis
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Cited articles

Allen, H. G.: Analysis and design of structural sandwich panels, Oxford, Pergamon Press, 1969. 
Bardell, N. S., Dunsdon, J. M., and Langley, R. S.: Free vibration analysis of coplanar sandwich panels, Compos. Struct., 38, 463–475, 1997. 
Chen, J. and Qiu, Q. Y.: Application and development of honeycomb sandwich structure on aircraft, New Materials Industry, 7, 63–67, 2018. 
Gibson, L. J., Ashby, M. F., Schajer, G. S., and Robertson, C. I.: The mechanics of two-dimensional cellular materials, Proc. R. Soc. Lon. A, 382, 25–42, 1982. 
Gunes, R. and Arslan, K.: Development of numerical realistic model for predicting low-velocity impact response of aluminum honeycomb sandwich structures, J. Sandw. Struct. Mater., 18, 95–112, 2016. 
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Short summary
Honeycomb sandwich (HS) structure has been widely used in aerospace applications because of its high specific strength and high specific stiffness. The structure of the lightweight HS panel is complex. Thus, establishing an equivalent simplified model is indispensable to improve the efficiency of the dynamic analysis of HS panels. In this paper, three commonly used dynamically equivalent modeling methods for HS panel are studied.