Transverse Shear Considerations in Anisotropic Plates
Abstract
This work was initiated by a need for solutions to a higher order shear deformation plate theory, which better approximates the through-the- thickness deformation and interlaminar shear stresses, using plates other than simply support. The non-simply support boundary conditions necessitated the Galerkin approximate technique. Solutions desired were natural frequencies and buckling loads for the following boundary conditions: simply supported, clamped, and clamped-simply support. Two graphite/epoxy laminates of different construction were investigated for effects of varying span-to-depth ratios. Comparisons of the higher order theory with linear and classical theory were made along with convergence characteristics of the Galerkin technique. Keywords: Composites, Plates, Vibrations, Buckling, Shear deformation, Galerkin technique.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1988
- Accession Number
- ADA203187
Entities
People
- Richard H. Reams
Organizations
- Air Force Institute of Technology