The Free Vibration Analysis of Honeycomb Sandwich Beam Using 3D and Continuum Model
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The Free Vibration Analysis of Honeycomb Sandwich Beam Using 3D and Continuum Model

Authors: G. Sakar, F. Ç. Bolat

Abstract:

In this study free vibration analysis of aluminum honeycomb sandwich structures were carried out experimentally and numerically. The natural frequencies and mode shapes of sandwich structures fabricated with different configurations for clamped-free boundary condition were determined. The effects of lower and upper face sheet thickness, the core material thickness, cell diameter, cell angle and foil thickness on the vibration characteristics were examined. The numerical studies were performed with ANSYS package. While the sandwich structures were modeled in ANSYS the continuum model was used. Later, the numerical results were compared with the experimental findings.

Keywords: Sandwich structure, free vibration, numeric analysis, 3D model, continuum model.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1107437

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References:


[1] ANSYS Online Help Documentation, ANSYS Inc.
[2] I. Aydıncak, “Investigation of design and analyses principles of honeycomb structures,” MSc. Thesis, METU, 2007.
[3] B. O. Baba, and R. F. Gibson, “The vibration response of composite sandwich beam with delamination,” Advanced Composite Letters, vol.16, pp.71-80, 2007.
[4] T. N. Bitzer, “Honeycomb Technology: Materials, design, manufacturing, applications and testing,” Chapman & Hall, 1997.
[5] G. Dai, and W. Zhang, “Cell Size Effects for Vibration Analysis and Design of Sandwich Beams,” Acta Mechanical Science, vol. 25, pp. 353-365, 2009.
[6] L. J. Gibson, and M. F. Ashby, “Cellular Solids-Structure and Properties,” Cambridge University Press, 1997.
[7] R. K. Khare, T. Kant, and A. A. Garg, “Free vibration of composite and sandwich laminates with a higher-order facet shell element”. Composite Structures, 65: 405–418. 2004.
[8] H. Y. Kim, and W. Hwang, “Effect of Debonding on Natural Frequencies and Frequency Response Functions of Honeycomb Sandwich Beams,” Composite Structures, vol. 55, pp. 51-61, 2002.
[9] L. Lai, “Study of Free Vibration of Aluminum Honeycomb Panels,” MSc. Thesis, Toronto University, 2002.
[10] Z. Li, and M.J. Crocker, “Effects of Thickness and Delamination on the Damping in Honeycomb–Foam Sandwich Beams,” Journal of Sound and Vibration, vol. 294, pp. 473–485, 2006.
[11] M.R. Maheri, and R.D. Adams, “Steady State Flexural Vibration Damping of Honeycomb Sandwich Beams,” Composite Science and Technology, vol. 52, pp. 333-347, 1994.
[12] E. Nilsson, and A. C. Nilsson, “Prediction and Measurement of Some Dynamic Properties of Sandwich Structures with Honeycomb and Foam Cores,” Journal of Sound and Vibration, vol. 251, pp. 409-430, 2002.
[13] M.K. Rao, and Y.M. Desai, “Analytical solutions for vibrations of laminated and sandwich plates using mixed theory,” Composite Structures, vol. 63, pp.361-373, 2004.
[14] T. Saito, R.D. Parbery, S. Okuno, and S. Kawano, “Parameter identification for Aluminum Honeycomb Sandwich Panels Based on Orthotropic Timoshenko Beam Theory,” Journal of Sound and Vibration, vol. 208, pp.271-287, 1997.
[15] Li. Yongqiang, and Z. Dawei, “Free flexural vibration analysis of symmetric rectangular honeycomb panel using the improved Reddy’s third-order plate theory,” Composite Structures, vol. 88, pp. 33–39, 2009.
[16] S.D. Yu, and W.L. Cleghorn, “Free Flexural Vibration Analysis of Symmetric Honeycomb Panels,” Journal of Sound and Vibration, vol. 284, pp. 189–204, 2005.
[17] W. X. Yuan, and D. J. Dawe, “Free vibration of sandwich plates with laminated faces,” International Journal for Numerical Methods in Engineering, vol. 54, pp. 195–217, 2002.