航空学报 > 1989, Vol. 10 Issue (3): 183-183

层板椭圆孔自由边缘效应

李明俊, 樊蔚勋   

  1. 南京航空学院
  • 收稿日期:1987-09-18 修回日期:1900-01-01 出版日期:1989-03-25 发布日期:1989-03-25

FREE EDGE EFFECT AROUND AN ELLIPTICAL HOLE IN A LAMINATE UNDER IN-PLATE LOADING

Li Minjun, Fan Weixun   

  1. Nanjing Aeronautical Institute
  • Received:1987-09-18 Revised:1900-01-01 Online:1989-03-25 Published:1989-03-25

摘要:

复合材料层板的直边和圆孔自由边缘效应的三维应力分析,国内外已有不少的数值解和近似解析解。Rybicki等提出了各向异性板椭圆孔2维问题变换为圆孔问题的方法,本文论证了这种变换方法的3维情形,从而可根据圆孔自由边缘效应结果来估计椭圆孔自由边缘效应。

关键词: 复合材料层板, 椭圆孔, 自由边缘效应, 三维应力

Abstract:

According to a method for transforming a three dimensional problem of a single elliptical hole in an anisotropic material to a problem of a circular hole in a different anisotropic material, we can treat the first boundary value problems in a laminate with an elliptical hole especially its free edge effect, if the problem with a circular hole has been solved.

Key words: composite laminate, elliptical hole, free edge effect, three dimensional stress