Free vibrations of laminated beams using mixed theory

Composite Structures

Volumn 52, Issue 2, 2001, Pages 149-160

  Kameswara Rao, M ^a   Desai, Y M ^a   Chitnis, M R ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY BOMBAY   (India)

Author keywords

Free vibrations; Laminated composite and sandwich beams; Mixed theory

Indexed keywords

BEAMS AND GIRDERS; NATURAL FREQUENCIES; SANDWICH STRUCTURES; SHEAR DEFORMATION; STIFFNESS MATRIX; STRESS ANALYSIS; STRUCTURAL ANALYSIS; VIBRATIONS (MECHANICAL);

HIGHER ORDER MIXED THEORY; LAMINATED BEAMS;

LAMINATED COMPOSITES;

LAMINATE; THEORETICAL ANALYSIS; VIBRATION;

EID: 0035340872     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00162-8     Document Type: Article

References (20)

1. On the correction for shear of differential equation for transverse vibrations of prismatic bars
2. Dynamic analysis of sandwich beams
3. Bending and vibration of multi ayer sandwich beams and plates
4. Free vibration of composite beams including rotary inertia and shear deformation
5. Vibration of symmetrically laminated clamped-free beam with a mass at the free end
6. A higher order beam finite element for bending and vibration problems
7. A new rectangular beam theory
8. Free vibration analysis of fiber reinforced composite beams using higher order theories and finite element modeling
9. Analytical solution to the dynamic analysis of laminated beams using higher order refined theory
10. Derivation of element stiffness matrices by assumed stress distributions
11. A new formulation of hybrid/mixed finite elements
12. A hybrid-stress finite element formulation for thick multilayer laminates
13. Hybrid-stress eight-node elements for thin and thick multilayer laminated plates
14. An invariant 8-node hybrid-stress element for thin and thick multilayer laminated plates
15. A three dimensional hybrid stress finite element formulation for free vibrations of laminated composite plates
16. A partial hybrid degenerated plate/shell element for the analysis of laminated composites
17. On the solution to the forced motions of rectangular composite plates
18. Nonlinear transient responses of initially stressed composite plates