Abstract
A novel solution of the free vibration problem formulated for a shallow sandwich cylindrical panel with fully clamped edges is presented in the paper. Based on this solution, an analytical formula for the fundamental frequency is derived. The panel vibrations are modelled using the engineering theory of laminated cylindrical shells taking into account the transverse shear deformations. The governing equations derived in terms of the panel displacements, deflections and angles of rotation of the normal element, are solved using the Galerkin method. The functions approximating the shape of the vibrating panel are obtained based on the analysis of the bending deformation of clamped–clamped sandwich beam subjected to a uniformly distributed inertial load. The analytical formula is applied to calculations of the fundamental frequencies for sandwich panels with various structural parameters. The results of these calculations have been successfully verified using the finite element method and implemented in the design analysis of sandwich panels considering a constraint imposed on the value of their fundamental frequency.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
