Analysis for delamination initiation in postbuckled dropped-ply laminates
- 13 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Delamination in tapered unidirectional glass fibre-epoxy under static tension loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Computational Structural Mechanics Methods Research Using an Evolving FrameworkPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Buckling and postbuckling of laminated composite plates with ply dropoffsAIAA Journal, 1989
- Quadratic Stress Criterion for Initiation of DelaminationJournal of Composite Materials, 1988
- Three-Dimensional Effective Elastic Constants for Thick LaminatesJournal of Composite Materials, 1988
- Tensile strength of tapered composite structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988