Hoff's Investigation of The Sandwich Panel with Honeycomb Core
Anbar Journal of Engineering Sciences,
2022, Volume 13, Issue 2, Pages 63-68
AbstractRecently, the use of sandwich panels has become increasingly important. This is due to its good mechanical properties and high strength-to-weight ratio. It is used in many fields, especially in aviation, construction and aerospace. It is necessary to know the behavior of the materials used, especially the free vibrations, to know the effect of external factors on the sandwich panels. The honeycomb core sandwich panel was studied. A model for analysis and modeling is proposed. A previous model was chosen for analysis and comparison. Hoff theory was applied to convert honeycomb sandwich panel into equivalent sandwich panel to facilitate the solution and save time. The limits were considered fixed on the one hand and moving on the other hand, and the ANSYS program was used to analyze and extract the results, and the results were compared and were promising and accurate, which proves to us the validity and accuracy of the proposed theoretical results
 Dung, L. V., Tien, D. L., & Minh, D. (2021). Numerical Simulation for the Honeycomb Core Sandwich Panels in Bending by Homogenization Method. Int. J. Mech, 15, 88-94.
 Dayyani, I., Ziaei-Rad, S., & Friswell, M. I. (2014). The mechanical behavior of composite corrugated core coated with elastomer for morphing skins. Journal of Composite Materials, 48(13), 1623-1636.
 Huang, S. N., & Alspaugh, D. W. (1974). Minimum weight sandwich beam design. AIAA Journal, 12(12), 1617-1618.
 A. Boudjemai, R. Amri, A. Mankour, H. Salem, M. H. Bouanane, and D. Boutchicha, “Modal analysis and testing of hexagonal honeycomb plates used for satellite structural design,” Materials and Design, vol. 35, pp. 266–275, 2015.
 W. H. Xie, S. H. Meng, F. Scarpa et al., “High-temperature high-velocity impact on honeycomb sandwich panels,” Composites Part B, vol. 138, pp. 1–11, 2018.
 D. Jeong, Y. Choi, and J. Kim, “Modeling and simulation of the hexagonal pattern formation of honeycombs by the immersed boundary method,” Communications in Nonlinear Science and Numerical Simulation, vol. 62, pp. 61–67, 2018.
 Allen, H. G. (1969). Analysis and structural design of sandwich panels.
 Gibson, I. J., & Ashby, M. F. (1982). The mechanics of three-dimensional cellular materials. Proceedings of the royal society of London. A. Mathematical and physical sciences, 382(1782), 43-59.
 L. J. Gibson and M. F. Ashby, Cellular Solids: Structure and Properties, Pergamon Press, Oxford, UK, 1998.
 Thompson, M. K., & Thompson, J. M. (2017). ANSYS mechanical APDL for finite element analysis. Butterworth-Heinemann.
 I. Aydıncak, “Investigation of design and analyses principles of honeycomb structures,” MSc. Thesis, METU, 2007.
 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.
 T. N. Bitzer, “Honeycomb Technology: Materials, design, manufacturing, applications and testing,” Chapman & Hall, 1997.
 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.
 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.
 Xu, Y., Wang, H., & Sheng, X. (2018). Multilayered equivalent finite element method for embedded honeycomb plates. Shock and Vibration, 2018.
 L.-J. Xia and X.-D. Jin, “+e equivalent analysis of honeycomb sandwich plates satellite structure,” Journal of Shanghai Jiao Tong University, vol. 37, no. 7, pp. 999–1001, 2003.
 Leissa, A. W. (1969). Vibration of plates (Vol. 160). Scientific and Technical Information Division, National Aeronautics and Space Administration..
 Sakata, T., & Hosokawa, K. (1988). Vibrations of clamped orthotropic rectangular plates. Journal of Sound and Vibration, 125(3), 429-439.
 Gorman, D. J. (1990). Accurate free vibration analysis of clamped orthotropic plates by the method of superposition. Journal of Sound and Vibration, 140(3), 391-411.
 Li, N. (1992). Forced vibration analysis of the clamped orthotropic rectangular plate by the superposition method. Journal of sound and vibration, 158(2), 307-316.
 Dalaei, M., & Kerr, A. D. (1996). Natural vibration analysis of clamped rectangular orthotropic plates. Journal of sound and vibration, 189(3), 399-406.
 Bercin, A. N. (1996). Free vibration solution for clamped orthotropic plates using the Kantorovich method. Journal of sound and vibration, 196(2), 243-247.
 Zhang, Z. J., Han, B., Zhang, Q. C., & Jin, F. (2017). Free vibration analysis of sandwich beams with honeycomb-corrugation hybrid cores. Composite Structures, 171, 335-344.
 De Gaetano, G., Cosco, F., Maletta, C., Garre, C., Donders, S., & Mundo, D. (2013). Innovative Concept Modelling of sandwich beam-like structures. In Proceedings of the 11th International Conference on Vibration Problems (pp. 1-10).
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