A first order, shear deformation plate theory is used to study the buckling speeds and the corresponding deformed shape of spinning, laminated composite plates offset from the axis of rotation. The theory accounts for geometric non-linearity in the form of von Kármán strains and the effects of rotat
VIBRATION CONTROL OF SHEAR DEFORMABLE LAMINATED PLATES—MODELING IMPLICATIONS
✍ Scribed by MIN-YUNG CHANG; LIVIU LIBRESCU
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 308 KB
- Volume
- 228
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
✦ Synopsis
A modal control approach is applied to control the vibration of homogeneous and laminated plates. The controller is designed using the linear optimal control theory. The performance of the controller designed according to a structural model of the plant based on the classical plate theory is evaluated and compared with that derived in the context of a higher order plate theory. It is found that the use of the classical plate model in the design of vibration control systems could lead to erroneous conclusions concerning the performance of the actual controlled system. The strong in#uence played by transverse shear deformation and lamination on the controlled system is clearly demonstrated and pertinent conclusions are outlined.
📜 SIMILAR VOLUMES
A previously published discrete-layer shear deformation theory is used to analyze free vibration of laminated plates. The theory includes the assumption that the transverse shear strains across any two layers are linearly dependent on each other. The theory has the same dependent variables as first
Using Reddy's higher order shear deformation plate theory, the #ow-induced vibrations of simply supported shear-deformable laminated plates exposed to an oscillating #ow are studied. The plate is assumed to be placed normal to the #ow. The #uid}structure interaction is based on Morison's model, whic
This paper presents di!erential quadrature solutions for free vibration analysis of moderately thick annular sector plates based on the Mindlin "rst-order shear deformation theory. Numerical characteristics of the di!erential quadrature method are illustrated through solving selected annular sector
A finite element formulation is presented to model the dynamic as well as static response of laminated composite plates containing integrated piezoelectric sensors and actuators subjected to both mechanical and electrical loadings. The formulation is based on the classical laminated plate theory and