Compressive behavior of honeycomb sandwich structure after impact

摘要：

　　The sandwich composite panel has the advantages of low density, large stiffness and especially obvious predominance in the flexural shear performance, so most of the aircraft structures, such as the floor and wings, are made of this kind of sandwich structure. However, the panel is usually thin and easily damaged under the impact of low energy, which has great influence on the bearing capacity of the structure.

关键词： compression honeycomb buckling sandwich impact

作者: Fei Xu Yage Liu Zhe Ji Yi Wang

作者单位: Department of Aeronautical Structure Engineering,Northwestern Polytechnical University,Xi’an 710072,China

会议类型: 国际会议

会议名称: 第13届国际断裂大会(ICF2013)

会议地点: 北京

会议语种:英文

页码: 1-1

在线出版日期: 2013-06-16（万方平台首次上网日期，不代表论文的发表时间）