Linear Parametric Vibrations of Sandwich Cylindrical Shell with Honeycomb Manufactured by FDM Additive Technology
Author:
Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-46874-2_20
Reference21 articles.
1. Yadav A, Amabili M, Panda SK et al (2021) Forced nonlinear vibrations of circular cylindrical sandwich shells with cellular core using higher-order shear and thickness deformation theory. J Sound Vib 510:116283. https://doi.org/10.1016/j.jsv.2021.116283
2. Zhang Y, Li Y (2019) Nonlinear dynamic analysis of a double curvature honeycomb sandwich shell with simply supported boundaries by the homotopy analysis method. Compos Struct 221:110884. https://doi.org/10.1016/j.compstruct.2019.04.056
3. Sadiq SE, Jweeg MJ, Bakhy SH (2020) The effects of honeycomb parameters on transient response of an aircraft sandwich panel structure. IOP Conf Ser Mater Sci Eng 928:022126. https://doi.org/10.1088/1757-899X/928/2/022126
4. Al-Khazraji MS, Jweeg MJ, Bakhy SH (2022) Free vibration analysis of a laminated honeycomb sandwich panel: a suggested analytical solution and a numerical validation. J Eng Des Technol (2022) https://doi.org/10.1108/JEDT-10-2021-0536
5. Sadiq SE, Bakhy S, Jweeg M (2021) Optimum vibration characteristics for honey comb sandwich panel used in aircraft structure. J Eng Sci Technol 16:1463–1479
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