An arbitrarily laminated, anisotropic cylindrical shell of finite length, under uniform internal pressure, is analyzed using Love-Timoshenko's kinematic relations and under the framework of classical lamination theory. The previously obtained solutions for asymmetrically laminated orthotropic (cross-ply) as well as unbalanced-symmetric and balanced-unsymmetric (angle-ply) cylindrical shells under the same loading conditions have been shown to be special cases of the present closed-form solution. Numerical results have been presented for a two-layer cylindrical shell and compared with those obtained using finite element solutions based on the layerwise constant shear-angle theory. These are expected to serve as benchmark solutions for future comparisons and to facilitate the use of unsymmetric lamination in design.
Arbitrarily laminated, anisotropic cylindrical shell under internal pressure
AIAA Journal ; 24
1986-11-01
Miscellaneous
No indication
English
Buckling of anisotropic laminated cylindrical plates
AIAA | 1983
|Buckling of anisotropic laminated cylindrical plates
AIAA | 1984
|