Intra-laminar fracture in angle-ply laminates
The development of matrix cracking in (0/θ/0) GFRP laminates, where θ = 45°, 54°, 75° and 90°, has been investigated. Crack initiation and propagation in the θ° ply were studied separately by using unnotched and notched samples. Details of average crack initiation/propagation strains and associated...
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Published in | Composites. Part A, Applied science and manufacturing Vol. 28; no. 9; pp. 839 - 846 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Oxford
Elsevier Ltd
1997
Elsevier |
Subjects | |
Online Access | Get full text |
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Summary: | The development of matrix cracking in (0/θ/0) GFRP laminates, where
θ = 45°, 54°, 75° and 90°, has been investigated. Crack initiation and propagation in the θ° ply were studied separately by using unnotched and notched samples. Details of average crack initiation/propagation strains and associated ply stresses, calculated from laminate theory, as functions of off-axis ply angle are presented and discussed for all laminates along with investigations of notch depth effects and crack growth patterns. It is suggested that to a first approximation crack propagation is governed by the transverse stress while crack initiation has a more complex and as yet unknown dependence on stress state. |
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Bibliography: | ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
ISSN: | 1359-835X 1878-5840 |
DOI: | 10.1016/S1359-835X(97)00036-5 |