Anisotropy-induced spiral buckling in compression-loaded cylindrical shells

AIAA Journal

Volumn 40, Issue 5, 2002, Pages 1001-1007

  Weaver, P M ^a  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPY; BENDING STRENGTH; BIFURCATION (MATHEMATICS); BUCKLING; DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; STRUCTURAL LOADS;

CYLINDRICAL SHELLS;

SHELLS (STRUCTURES);

EID: 0036572764     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1740     Document Type: Article

References (18)

1. The effect of flexural-twist anisotropy on compression buckling of quasi-isotropic laminated cylindrical shells
2. Effects of boundary conditions on the stability of cylinders subject to lateral and axial pressures
3. Interactive local/euler buckling of orthotropic cylindrical shells
4. Optimal laminate configuration of cylindrical shells for axial buckling
5. Stiffness optimization of orthotropic laminated composites using lamination parameters
6. Importance of anisotropy on buckling of composite-loaded symmetric composites plates
7. An assessment of shell theories for buckling of circular cylindrical panels loaded in compression
8. Computation of localised post buckling of long axially compressed cylinders
9. Computation of homoclinic orbits in partial differential equations: An application to cylindrical shell buckling
10. Critical stresses of thin-walled cylinder in torsion
11. Anisotropic effects in the compression buckling of laminated composite cylindrical shells
12. Effect of imperfections on the buckling response of compression: Loaded shells