Based on a higher order plate theory, non-linear partial differential equations for the vibrating motion of a plate are derived. By using these equations, the large amplitude vibration of a simply supported rectangular plate is investigated. By neglecting the higher order terms and introducing the s
Large amplitude vibration of a beam based on a higher-order deformation theory
โ Scribed by Ji-Liang Doong; Chun-Sheng Chen
- Publisher
- Elsevier Science
- Year
- 1988
- Tongue
- English
- Weight
- 552 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0003-682X
No coin nor oath required. For personal study only.
โฆ Synopsis
A BSTRA CT A higher-order formulation of large amplitude vibrations of simply supported beams subjected to initial stress is presented. The initial stress is taken to be a combination of a pure bending stress plus an extensional stress of the neutral axis of the beam. By neglecting the higher-order terms and introducing the shear correction factor into governing equations, these equations can be reduced to Timoshenko beam theory ( present first-order beam theory). The Galerkin method is used to reduce the governing nonlinear partial differential equations to ordinary nonlinear differential equations in terms o fan unknown function of time. The Runge-Kutta method is. used to obtain the period. Numerical results show that if the amplitude ratio increases, significant errors in the first-order beam theory can be observed, and that higher-order shear deformation terms are necessary to solve this problem.
๐ SIMILAR VOLUMES
A new one-dimensional theory is presented for studying the static and vibration behavior of cylindrical or prismatic beam-type structures. This general higher order theory, which is developed for beams having an arbitrary cross-section, accurately accounts for transverse shear deformation out of the
This paper presents a new finite element formulation for the free vibration analysis of composite beams based on the third-order beam theory. This work also studies the influence of the mass components resulting from higher-order displacements on the frequencies of flexural vibration. By using Hamil
Natural frequencies and buckling stresses of laminated composite beams are analyzed by taking into account the complete e!ects of transverse shear and normal stresses and rotatory inertia. By using the method of power series expansion of displacement components, a set of fundamental dynamic equation