In order to accurately determine the dynamic response of cross-ply laminated thick plates subjected to moving load, a solution procedure based on the three-dimensional (3D) elasticity theory is presented. Plates with simply supported edges and subjected to point moving load are considered. The layer
Three-dimensional contact dynamics of laminated plates:: Part 1. Normal impact
โ Scribed by C.C. Chao; C.Y. Tu
- Book ID
- 104404393
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 549 KB
- Volume
- 30
- Category
- Article
- ISSN
- 1359-8368
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โฆ Synopsis
The Hertzian static contact law predicts the force-indentation relationship for impacted composite laminates inaccurately. An innovative solution method has been developed for the impact contact problem by using volumetric displacements as control variables and discrete patch loadings as state variables. Impact responses are acquired through modal superposition in terms of loading distribution rather than conventional displacement fields. A system of governing equations of contact stresses is derived via an energy variational approach, with three-dimensional boundary conditions and interlaminar continuity taken into account. Using small incremental linearization, the nonlinear impact contact problem involving discrete pressures and the final contact area is solved by iteration. Three-dimensional displacements and stresses can be evaluated throughout the laminated plate for dynamic response.
๐ SIMILAR VOLUMES
As far as the dynamics of multibody systems is concerned, a brief review has been performed in order to frame the dynamic response of a trilith (the simplest scheme of a colonnade belonging to a temple) into a wide theoretical background. Under the assumption of rigid bodies, two di!erent approaches