A partial hybrid plate element vibration analysis is established for orthotropic laminated plates. The inertia effect is considered by adding kinetic energy to the modified HellingerReissner principle. The dynamic governing equations of the plate are then derived variationally. As the through-thickn
A PARTIAL HYBRID DEGENERATED PLATE/SHELL ELEMENT FOR THE ANALYSIS OF LAMINATED COMPOSITES
β Scribed by W. FENG; S. V. HOA
- Publisher
- John Wiley and Sons
- Year
- 1996
- Tongue
- English
- Weight
- 683 KB
- Volume
- 39
- Category
- Article
- ISSN
- 0029-5981
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β¦ Synopsis
A degenerated plate/shell element based on the combined energy variational principle and the equivalent single-layer model is proposed. It is derived from the 3-D continuum equation by imposing one constraint on the 3-D isoparametric solid element: a straight line normal to the mid-surface before deformation remains straight but not normal after deformation. The continuities of interlaminar stresses are satisfied at the interlaminar surface and the number of degrees of freedom per node is independent of the number of layers. In this work, the combined energy variational principle is used to overcome transverse stress continuity limitations of single-layer models. The traction-free conditions are satisfied on the upper and lower surfaces of a laminate by assuming the transverse stress components independently. The transverse normal strain is taken into account in order to consider the full 3-D effect in a laminated composite. The iso-function method and the classification method of the stress modes are used to construct the assumed stress field which contains a minimum number of stress modes and guarantees no zero energy mode in the element stiffness matrix. Three examples are presented to illustrate the efficiency and accuracy of the element.
π SIMILAR VOLUMES
This paper presents a new 4-node ΓΏnite-element for the analysis of laminated composite plates. The element is based on a ΓΏrst-order shear deformation theory and is obtained through a mixed-enhanced approach. In fact, the adopted variational formulation includes as variables the transverse shear as w
## Abstract Two simple 4βnode 20βDOF and 4βnode 24βDOF displacementβbased quadrilateral elements named RDKQβL20 and RDKQβL24 are developed in this paper based on the firstβorder shear deformation theory (FSDT) for linear analysis of thin to moderately thick laminates. The deflection and rotation fu