航空学报 > 1991, Vol. 12 Issue (12): 623-627

含孔层合板考虑边界效应的拉伸强度分析

李顺林, 熊中侃   

  1. 南京航空学院
  • 收稿日期:1991-02-23 修回日期:1991-06-10 出版日期:1991-12-25 发布日期:1991-12-25

ANALYSIS OF TENSILE STRENGTH OF LAMINATES WITH A HOLE TAKING INTO ACCOUNT THE EDGE-EFFECT

Li Shunlin, Xiong Zhongkan   

  1. Nanjing Aeronautical Institute
  • Received:1991-02-23 Revised:1991-06-10 Online:1991-12-25 Published:1991-12-25

关键词: 含孔层合板, 有限宽层合板, 边界效应, 拉伸强度, 复合材料

Abstract: An analysis of the tensile strength of [0/90]5, C45/ - 45]5, and π/4 laminates with a hole of various finite width and the hole diameter is presented. It is found that, the tensile strength of laminates with a hole relates to not only material property, geometry size of sample, but also ply condition. A strength calculate formulation and a method of modification is also given to allow for the edge-effect of the general symmetrical π/4 laminates with a hole. This is an empirical approach based on the result of experiments. This approach is different compared to former approaches based on model for strength of materials or fracture mechanics. It is a approach based on model for mechanics of composite materials, which considered ply-condition of composite materials.

Key words: laminates with a hole, laminates of finite width, edge-effect, tensile strength, composite materials