Fatigue behavior of foam core sandwich beams with sub-interface impact damage

被引:9
|
作者
Shipsha, A [1 ]
Zenkert, D [1 ]
机构
[1] Royal Inst Technol, Dept Aeronaut, S-10044 Stockholm, Sweden
关键词
FAILURE MECHANISMS; CRACK-PROPAGATION; SHEAR PROPERTIES; 2D APPROACH; COMPOSITE; GROWTH;
D O I
10.1177/1099636203005002906
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The fatigue life of impact-damaged foam core sandwich beams with GFRP faces is investigated for constant load-amplitude cyclic loading. The damage produced by the low velocity/energy impact is characterised as a sub-interface cavity with surrounding crushed core whereas the face sheet is undamaged. The effect of bridging owing to the crushed core in the peripheral regions of impact damage, revealed in the preceding static study Shipsha et al. [1,2] is assessed under cyclic loading. The fatigue test results are analysed in a stress-life S-N diagram and compared with published data from undamaged beams. The effect of two load ratios R = 0.1 and -1 is investigated. The fatigue threshold load levels are experimentally quantified from the S-N curves. Furthermore, a modified point-stress criterion based on the threshold stress intensity factor, K-th, is proposed to estimate the "no-crack growth" limit loads. The results show good agreement with performed experiments.
引用
收藏
页码:147 / 160
页数:14
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