FATIGUE BEHAVIOR OF STITCHED GRP LAMINATES

Citation
Mzs. Khan et Ap. Mouritz, FATIGUE BEHAVIOR OF STITCHED GRP LAMINATES, Composites science and technology, 56(6), 1996, pp. 695-701
Citations number
30
Categorie Soggetti
Materials Sciences, Composites
ISSN journal
02663538
Volume
56
Issue
6
Year of publication
1996
Pages
695 - 701
Database
ISI
SICI code
0266-3538(1996)56:6<695:FBOSGL>2.0.ZU;2-J
Abstract
This paper examines the effect of through-thickness stitching on the i n-plane fatigue performance and fatigue damage mechanisms of a glass-r einforced polymer (GRP) laminate under zero-to-tension cyclic loading The influence of stitching orientation and stitching density on the S- N curve of the laminate has also been investigated. The fatigue resist ance was reduced considerably by stitching, particularly at relatively low fatigue stresses. Both the non-stitched and stitched laminates ex perienced similar types of fatigue damage, i.e. cracking of the vinyl ester resin matrix and glass fibres, and debonding between the matrix and fibres. However, the stitched laminates also suffered fatigue fail ure between the stitches and surrounding laminate, which contributed t o the reduction in the fatigue lives of these materials. Their fatigue resistance was also reduced by damage to the glass fibres caused when the laminates were stitched. It was concluded that while stitching im proved the interlaminar fracture properties of the GRP, it seriously d egraded the fatigue performance. (C) 1996 Published by Elsevier Scienc e Limited