delamination;
mixed-mode bending;
finite-element analysis;
beam theory model;
fracture loci;
D O I:
10.1007/s11029-007-0023-1
中图分类号:
O3 [力学];
学科分类号:
08 ;
0801 ;
摘要:
The mixed-mode I + II interlaminar fracture of multidirectional glass/epoxy laminates is investigated. Mixed-mode bending (MMB) tests were performed on specimens with delaminations in 0/theta-type interfaces, with theta varying from 0 to 90 degrees. Preliminary three-dimensional finite-elementanalyses validated the beam theory model (BTM) used for analysing experimental data. The compliances measured are in a good agreement with BTM predictions. The total critical energy release rate GC varies linearly with the mode II ratio G(II)/G, although some discrepancies are observed in the high-mode II results for the 0/45 and 0/90 specimens.
机构:
USAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USAUSAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USA
Kim, BW
;
Mayer, AH
论文数: 0引用数: 0
h-index: 0
机构:
USAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USAUSAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USA
机构:
USAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USAUSAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USA
Kim, BW
;
Mayer, AH
论文数: 0引用数: 0
h-index: 0
机构:
USAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USAUSAF, Res Lab, Air Vehicle Directorate, Struct Design & Dev Branch, Wright Patterson AFB, OH 45433 USA