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contributor authorQingyuan Chen
contributor authorPizhong Qiao
date accessioned2025-08-17T22:30:26Z
date available2025-08-17T22:30:26Z
date copyright1/1/2025 12:00:00 AM
date issued2025
identifier otherJAEEEZ.ASENG-5693.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307030
description abstractAn approximate explicit analytical solution to the free vibration behavior of orthotropic plates with all edges rotationally restrained against rotation based on the deformation shape function and the Galerkin method is presented. The deformation shape function along each direction is uniquely constructed through a weighted combination of vibration characteristic functions of simply supported-clamped beam and modified vibration characteristic functions of clamped-simply supported beam and clamped-clamped beam to meet the elastically restrained opposite edges against different rotation; whereas to satisfy the elastically restrained opposite edges against the same rotation, the deformation shape function along each direction is chosen by combining the vibration characteristic function of simply supported beam and the modified vibration characteristic function of clamped-clamped beam. It is revealed that the present approximate explicit analytical solution can avoid possible numerical instabilities in the method based on the classical vibration characteristic function of beam and is effective and accurate for performing the free vibration analysis of orthotropic plates with all the opposite edges arbitrarily elastically restrained against rotation.
publisherAmerican Society of Civil Engineers
titleExplicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates
typeJournal Article
journal volume38
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-5693
journal fristpage04024112-1
journal lastpage04024112-18
page18
treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 001
contenttypeFulltext


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