Interlaminar stress analysis of laminated composite beams according to global higher-order deformation theories

Composite Structures

Volumn 55, Issue 1, 2002, Pages 105-114

  Matsunaga, Hiroyuki ^a  

^a SETSUNAN UNIVERSITY   (Japan)

Author keywords

Laminated composite beams; Single layer higher order beam theory; Stress and displacement distributions

Indexed keywords

BOUNDARY VALUE PROBLEMS; DEFORMATION; ELASTICITY; INTERFACES (MATERIALS); LAMINATED COMPOSITES; SHEAR STRESS; STRESS ANALYSIS;

INTERLAMINAR STRESS ANALYSIS;

COMPOSITE BEAMS AND GIRDERS;

COMPOSITE; DEFORMATION; ELASTICITY; INTERLAMINAR PROPERTY; STRESS; THEORY;

EID: 0036139630     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00134-9     Document Type: Article

References (12)

1. Exact solutions for composite laminates in cylindrical bending
2. Exact solutions for rectangular bidirectional composites
3. 1993 Modelling of thick composites using a layerwise laminate theory
4. o zig-zag finite element for analysis of laminated composite beams
5. Free vibration and stability of thin elastic beams subjected to axial forces
6. Buckling instabilities of thick elastic beams subjected to axial stresses
7. Vibration and buckling of deep beam-columns on two-parameter elastic foundations
8. Vibration and stability of cross-ply laminated composite plates according to a global higher-order plate theory
9. An interlaminar stress continuity theory for laminated composite analysis
10. Laminated composite plate theory with improved in-plane responses
11. Thick beam theory and finite element model with zig-zag sublaminate approximations