Abstract
A nonlinear material constitutive model, including a nonlinear in-plane shear formulation and a failure criterion, for fiber-composite laminate materials is employed to carry out finite-element buckling analyses for composite shells under hydrostatic compressive loads. It has been shown that the nonlinear in-plane shear together with the failure criterion have significant influence on the buckling behavior of composite shells.
Original language | English |
---|---|
Pages (from-to) | 202-208 |
Number of pages | 7 |
Journal | Journal of Composites Technology and Research |
Volume | 15 |
Issue number | 3 |
DOIs | |
Publication status | Published - 1993 Jan 1 |
All Science Journal Classification (ASJC) codes
- Ceramics and Composites
- Polymers and Plastics
- Materials Chemistry