Abstract
Composite materials are prone to a wide range of defects and damage which may significantly reduce their residual strength. Of the various types of defects possible, interply delaminations arising from in-service damage are probably the most insiduous because of their effects on residual compressive strength and difficulties associated with their detection. In this study, a finite element analysis of the self similar growth of a circular delamination in a compressed laminate is undertaken, and the results are compared with an analytical solution.
Original language | English |
---|---|
Pages (from-to) | 99-104 |
Number of pages | 6 |
Journal | Theoretical and Applied Fracture Mechanics |
Volume | 13 |
Issue number | 2 |
DOIs | |
Publication status | Published - May 1990 |
Externally published | Yes |