A high order shear deformation theory is used to develop a discrete model for the sensitivity analysis and optimization of laminated plate and shell structures in non-linear response. The geometrically non-linear analysis is based on an updated Lagrangian formulation associated with the NewtonยฑRaphs
Linear and geometrically nonlinear vibrations of fiber reinforced laminated plates and shallow shells
โ Scribed by A.V. Singh
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 385 KB
- Volume
- 76
- Category
- Article
- ISSN
- 0045-7949
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โฆ Synopsis
This paper deals with the free ยฏexural vibration of laminated quadrilateral plates and shallow shells using the RayleighยฑRitz method. Equations are derived using the ยฎrst order shear deformation theory of plates and shells. Nonlinearity is present only in the in-plane strain components. The transverse shear strains, curvature and inertial terms are linear. The geometry is mapped using the natural coordinates. Admissible displacement ยฎelds are constructed by taking the product of two simple polynomials in each of the two parametric coordinates. By controlling the coecients of these polynomials, the geometric boundary conditions are satisยฎed. Numerical results are presented for the four-layer angle-ply plates and cylindrical shallow shells supported on trapezoidal boundary. The inยฏuences of the large amplitude and also of the geometry on the natural frequency are examined.
๐ SIMILAR VOLUMES
In this paper, the nonlinear equations of motion for laminated composite rectangular plates based on first order shear deformation theory, which include shear deformation and rotary inertia, have been derived. Then, through introducing a force function, these equations reduced to a set of coupled no