Experiment and Simulation on Natural Frequency of Fiber-Paper Honeycomb Sandwich Structure Composites

Yang, Xiao Jun; Lan, Qing Shan; Zhong, Yu Ning

doi:10.4028/www.scientific.net/AMM.101-102.360

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Home Applied Mechanics and Materials Advances in Engineering Design and Optimization IIExperiment and Simulation on Natural Frequency of...

Experiment and Simulation on Natural Frequency of Fiber-Paper Honeycomb Sandwich Structure Composites

Abstract:

The theory of natural frequencies were acquired from vibration experiment, meanwhile, the first order frequencies of honeycomb sandwich structure composites were obtained by using the sandwich laminboard theory and equivalent panel theory via the finite element software ANSYS. The simulation results were compared to the experiment results to get the error of calculation of the two different equivalent methods, thereby we can select more appropriate equivalent method to ensure the veracity of the result analysis and provide a reference for the optimization design of the fiber-paper honeycomb sandwich structure composites.

Info:

Periodical:

Applied Mechanics and Materials (Volumes 101-102)

Main Theme:

Advances in Engineering Design and Optimization II

Edited by:

Di Zheng, Yiqiang Wang, Yi-Min Deng, Aibing Yu and Weihua Li

Pages:

360-364

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.101-102.360

Citation:

X. J. Yang et al., "Experiment and Simulation on Natural Frequency of Fiber-Paper Honeycomb Sandwich Structure Composites", Applied Mechanics and Materials, Vols. 101-102, pp. 360-364, 2012

Online since:

September 2011

Authors:

Xiao Jun Yang, Qing Shan Lan, Yu Ning Zhong

Keywords:

Finite Element, Honeycomb Sandwich Structure Composites, Natural Frequency

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$38.00

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References

[1] S. Ontaç, S. Dağ and M.I. Gökler: 3rd International Conference on Recent Advances in Space Technologies (Istanbul, Turkey, June 14-16, 2007). vol. 1, pp.171-175.

[2] A. Boudjemai, M.H. Bouanane, L. Merad and A.M. Si Mohammed: 3rd International Conference on Recent Advances in Space Technologies (Istanbul, Turkey, June 14-16, 2007). vol. 1, pp.398-406.

DOI: https://doi.org/10.1109/rast.2007.4284021

[3] D.P. Zhu, S.S. Zhou: 2008 International Conference on Computer Science and Software Engineering ( Wuhan, China, December 12-14, 2008). vol. 6, pp.417-420.

[4] J. Liu, Y.J. Lv: 2009 IEEE 10th International Conference on Computer-Aided Industrial Design & Conceptual Design (Wenzhou, China, November 26-29, 2009). vol. no, pp.2166-2169.

[5] H.T. Wei, X.R. Kong: 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (Harbin, China, June 8-10, 2010). vol. no, pp.478-482.

[6] Z.F. Bai, Y. Zhao, W.L. Ma and H. Tian: 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics (Harbin, China, December 10-12, 2008). vol. no, pp.1-5.

[7] Y. Tanimoto, T. Nishiwaki, T. Shiomi and Z. Maekawa: Composite Interfaces, Vol. 8 (2001) No. 6, p.393–402.

[8] M.H. Fu, J.R. Yin: Acta Mechanica Sinica, Vol. 31, (1999) No. 1, pp.113-118(In Chinese).

[9] L.J. Gibson, M.F. Ashby, P.S. Liu: Cellular Solids: Structure and Properties (Second Edition) (Beijing: Tsinghua University Press, China 2003).

[10] C.Z. Zhang: the Mechanical Analytic Theory of Composite Laminated Plate and Shell (Beijing: National Defense Industry Press, China 2009).

Paper TitlePages

Mechanical Property Analysis and Numerical Simulation of Honeycomb Sandwich Structure’s Core

Authors: Xiang Li, Min You

Abstract: Owing to the lack of a good theory method to obtain the accurate equivalent elastic constants of hexagon honeycomb sandwich structure’s core, the paper analyzed mechanics performance of honeycomb sandwich structure’s core and deduced equivalent elastic constants of hexagon honeycomb sandwich structure’s core considering the wall plate expansion deformation’s effect of hexagonal cell. And also a typical satellite sandwich structure was chose as an application to analyze. The commercial finite element program ANSYS was employed to evaluate the mechanics property of hexagon honeycomb core. Numerical simulation analysis and theoretical calculation results show the formulas of equivalent elastic constants is correct and also research results of the paper provide theory basis for satellite cellular sandwich structure optimization design.

518

The Main Factors that Influence the Mechanical Properties of Honeycomb Board

Authors: Cong Bo Ma, Yan Wei Wang, Guang Ping Zou, Xuan Du

Abstract: It’s very important to select appropriate dimensions for manufacture of honeycomb sandwich. In this paper, the experimental and theoretical methods were compared. The results are proved that the theoretical formula can be applied to engineering design. The impact factor of staties mechanical properties of honeycomb panels also was studied. And a theoretical basis for the design of honeycomb sandwich panels is provided.

812

Dynamic Analysis of Sandwich Plate Structure by Finite Element Method

Authors: Amit Paul, Sreyashi Das Nee Pal, Arup Guha Niyogi

Abstract: An 8-noded quadratic isoparametric plate bending finite element that incorporates first-order transverse shear deformation and rotary inertia is used to predict the free vibration response of sandwich plate structures. A programme has been developed using MATLAB. The finite element results presented here show good agreement with the available semi-analytical solutions and finite element results. Parametric studies have been conducted by incorporating variation in support conditions, fibre angles of the skins and overall thickness and detail interpretations are provided.

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