Stability and vibration of isotropic, orthotropic and laminated plates according to a higher-order shear deformation theory
β Scribed by J.N. Reddy; N.D. Phan
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 793 KB
- Volume
- 98
- Category
- Article
- ISSN
- 0022-460X
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π SIMILAR VOLUMES
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
A higher-order shear deformation theory is used to analyse laminated anisotropic composite plates for deflections, stresses, natural frequencies and buckling loads. The theory accounts for parabolic distribution of the transverse shear stresses, and requires no shear correction coefficients. A displ
Laminated composite plates are being increasingly used in the aeronautical and aerospace industry as well as in other "elds of modern technology. To use them e!eciently a good understanding of their structural and dynamical behaviour is needed. The Classical ΒΈaminate Plate ΒΉheory [1] which ignores t
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