Free Vibrations Analysis of a Functionally Graded Honeycomb (FGH) Sandwich Cylindrical Shell Using a Quasi-3D Theory
This paper examines the free vibration behavior of functionally graded (FG) hexagonal honeycomb sandwich cylindrical shells using a quasi-3D theory. The material properties are assumed to vary continuously through the thickness, following a power-law distribution that ranges from zero at the inner surface to one at the outer surface. Shear deformation and thickness stretching effects are captured by modeling all displacement fields with a hyperbolic distribution through the thickness. The governing equations are derived using Hamilton’s principle, and natural frequencies are calculated via the Navier technique. The accuracy of the hybrid quasi-3D theory is validated through comparisons with existing literature. Additionally, the influence of material and geometric parameters on natural frequencies is investigated within this framework.
Authors
- Abdelouahed Tounsi (ORCID: https://orcid.org/0000-0002-5601-3228)
- Hadj Youzera (ORCID: https://orcid.org/0009-0007-8181-8988)
- Mahmoud M. Selim (ORCID: https://orcid.org/0000-0002-9727-4520)
- Sherain M.Y. Mohamed
Institutions
- King Fahd University of Petroleum and Minerals (SA)
- Prince Sattam Bin Abdulaziz University (SA)
- Université Mustapha Stambouli de Mascara (DZ)
- Université Djilali de Sidi Bel Abbès (DZ)
Publication Details
- Journal
- International Journal of Structural Stability and Dynamics
- Published
- 2025-11-21
- DOI
- https://doi.org/10.1142/s0219455427501598
- Primary Topic
- Composite Structure Analysis and Optimization
- Type
- article
- Field-Weighted Citation Impact
- 0.00