Modal Analysis of Honeycomb Core Sandwich Panel Using Finite Element Method
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-93377-7_6
Reference18 articles.
1. Boudjemai, A., Amri, R., Mankour, A., Salem, H., Bouanane, M.H., Boutchicha, D.: Modal analysis and testing of hexagonal honeycomb plates used for satellite structural design. Mater. Des. 35, 266–275 (2012). https://doi.org/10.1016/j.matdes.2011.09.012
2. Crupi, V., Epasto, G., Guglielmino, E.: Comparison of aluminium sandwiches for lightweight ship structures: honeycomb versus foam. Mar. Struct. 30, 74–96 (2013). https://doi.org/10.1016/j.marstruc.2012.11.002
3. Sun, G., Huo, X., Wang, H., Hazell, P.J., Li, Q.: On the structural parameters of honeycomb-core sandwich panels against low-velocity impact. Compos. Part B: Eng. 216, 108881 (2021). https://doi.org/10.1016/j.compositesb.2021.108881
4. Jin, Y., Shi, Y., Yu, G.-C., Wei, G.-T., Hu, B., Wu, L.-Z.: A multifunctional honeycomb metastructure for vibration suppression. Int. J. Mech. Sci. 188, 105964 (2020). https://doi.org/10.1016/j.ijmecsci.2020.105964
5. Ng, C.F., Hui, C.K.: Low frequency sound insulation using stiffness control with honeycomb panels. Appl. Acoust. 69(4), 293–301 (2008). https://doi.org/10.1016/j.apacoust.2006.12.001
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