FAILURE CHARACTERISTICS OF GRAPHITE-EPOXY STRUCTURAL COMPONENTS LOADED IN COMPRESSION

Publisher Website

1 January 1983

book chapter
Published by Elsevier

p. 283-306
https://doi.org/10.1016/b978-0-08-029384-4.50025-0

Abstract

No abstract available

Keywords

This publication has 7 references indexed in Scilit:

Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
Effect of orthotropic properties and panel width on the compression strength of graphite-epoxy laminates with holes
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compression
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
One dimensional modelling of failure in laminated plates by delamination buckling
International Journal of Solids and Structures, 1981
Effect of Impact Damage and Holes on the Compressive Strength of a Graphite/Epoxy Laminate
Published by ASTM International ,1979
Analytical and experimental study of structurally efficient composite hat-stiffened panels loaded in axial compression
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations
Journal of Composite Materials, 1974