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 inComposites. Part A, Applied science and manufacturing Vol. 28; no. 9; pp. 839 - 846
Main Authors Crocker, L.E., Ogin, S.L., Smith, P.A., Hill, P.S.
Format Journal Article
LanguageEnglish
Published Oxford Elsevier Ltd 1997
Elsevier
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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.
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