Nonlinear dynamic finite element analysis of composite cylindrical shells considering large rotations

Citation
Lnb. Gummadi et An. Palazotto, Nonlinear dynamic finite element analysis of composite cylindrical shells considering large rotations, AIAA J, 37(11), 1999, pp. 1489-1494
Citations number
20
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
37
Issue
11
Year of publication
1999
Pages
1489 - 1494
Database
ISI
SICI code
0001-1452(199911)37:11<1489:NDFEAO>2.0.ZU;2-3
Abstract
A new nonlinear finite element formulation is developed for the nonlinear d ynamics of shell structures. Using a vectorial approach, the kinematics tha t can be used to describe very large displacements and large rotations are derived. Green strain measures and second Piola Kirchhoff stress measures a re used in the determination of the total potential. A displacement-based e ight-noded cylindrical shell element with a total of 36 degrees of freedom is developed. Several numerical examples are dynamically analyzed to observ e the characteristics of large displacements and large rotations. A converg ence study was carried out to establish the numerical accuracy of the model . The most efficient and accurate model was used.