A semi-analytical finite element for laminated composite plates

Composite Structures

Volumn 57, Issue 1-4, 2002, Pages 117-123

  Sheng, H Y ^a   Ye, J Q ^b  

^a HEFEI UNIVERSITY OF TECHNOLOGY   (China)

^b UNIVERSITY OF LEEDS   (United Kingdom)

Author keywords

Finite element; Laminated composite plate; State equation; Three dimensional elasticity

Indexed keywords

ALGEBRA; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; THICKNESS MEASUREMENT;

MIXED VARIATIONAL PRINCIPLE;

COMPOSITE STRUCTURES;

COMPOSITE;

EID: 0036659734     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00075-2     Document Type: Article

References (11)

1. Bending vibration and buckling of simply supported thick orthotropic rectangular plates and laminates
2. An exact three-dimensional solution for normal loading of inhomogeneous and laminated anisotropic elastic plates of moderate thickness
3. An exact solution for the statics and dynamics of laminated thick plates with orthotropic layers
4. Three-dimensional solution of the free vibration problem of homogeneous isotropic cylindrical shells and panels
5. Exact solution for thick laminates with clamped edges
6. Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports
7. A free vibration analysis of cross-ply laminated rectangular plates with clamped edges
8. Stress, vibration, and buckling of multilayered cylinders
9. Assessment of computational models for of multi-layered composite shells
10. An evaluation of equivalent-single-layer and layerwise theories of composite laminates