Compressive failure of impacted NCF composite sandwich panels - Characterisation of the failure process

被引:45
作者
Edgren, F
Asp, LE
Bull, PH
机构
[1] SICOMP AB, SE-43122 Molndal, Sweden
[2] Royal Inst Technol, Dept Aeronaut, SE-10044 Stockholm, Sweden
关键词
damage tolerance; fractography; CFRP; sandwich; CAI;
D O I
10.1177/0021998304040559
中图分类号
TB33 [复合材料];
学科分类号
摘要
In the present study, non-crimp fabric (NCF) composite face sheet sandwich panels have been tested in compression after impact (CAI). Damage in the face sheets was characterised by fractography. Compression after impact loaded panels were found to fail by plastic fibre microbuckling (kinking) in the damaged face sheet. Studies of panels for which loading was interrupted prior to failure revealed extensive stable kink band formation at several positions and in numerous plies. Kink bands initiated and propagated within a wide region close to the point of impact. In addition, kink bands initiated in zones with high shear stresses, away from the impact centre line. Consequently, the fractographic results from this investigation do not support the assumption of modelling the impact damage as an equivalent hole. To achieve accurate predictions of kink band initiation, the stress field must be known. The results from this study imply that bending effects caused by remaining dent or material eccentricities in the damaged region must be considered.
引用
收藏
页码:495 / 514
页数:20
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