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 evaluat
Stability of Spinning Shear-Deformable Laminated Composite Plates
β Scribed by R. Bhumbla; J.B. Kosmatka
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 469 KB
- Volume
- 163
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
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 KΓ‘rmΓ‘n strains and the effects of rotatory inertia. A displacement finite element model is developed to obtain the numerical solutions to this class of problems. The buckling speeds are presented as functions of spin vector location and orientation (pitch and precone), and composite ply lay-up. The phenomenon of tensile buckling is examined. The buckling speed is seen to decrease with the spin vector offset from the plate clamped root, and increasing pitch orientation. It is shown that laminated plates can be designed to buckle in specific modes and at specific speeds. Non-linear effects have been shown to be significant for cases where there is coupling between in-plane and out-of-plane deflections of the plate. This coupling is a result of either material anisotropy or the application of forces out of plane of the plate.
π SIMILAR VOLUMES
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
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