The Non-Linear Dynamics of Composite Cylindrical Shells
Abstract
The non-linear dynamic behavior of suddenly loaded composite shells is the subject of this research. The objective of research is two-fold: (1) to characterize the apparently random physical behavior sometimes observed in the finite element analysis as either numerical instability, chaotic behavior, or both; and (2) to develop criteria for choosing time steps for the finite element model, referred to as DSHELL. This displacement based finite element code is capable of dynamic analysis of plates, arches, and cylindrical shells undergoing large displacements and moderately large rotations during deformation. DSHELL uses a 36-DOF isoparametric shell element to obtain numerical results. A simplified shell model (MSHELL) is developed to provide a shell analog that requires much less computer time to run than the full-up
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 15, 1992
- Accession Number
- ADA259026
Entities
People
- James M. Greer Jr.
Organizations
- Air Force Institute of Technology