FREE-EDGE STRESS REDUCTION THROUGH FIBER VOLUME FRACTION VARIATION

被引:14
作者
SHIAU, LC
CHUE, YH
机构
[1] Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan
关键词
Fiber Volume Fraction Variation - Free Edge Interlaminar Stresses - Free Edge Stress Reduction - Uniform Axial Extension;
D O I
10.1016/0263-8223(91)90020-Y
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An effective technique to reduce the free-edge interlaminar stresses in a symmetric laminate under uniform axial extension is presented. A pseudo three-dimensional finite element method is employed to calculate the interlaminar stresses. The reduction of the interlaminar stresses is achieved by varying the fiber volume fraction near the free edge. Numerical results show that the interlaminar normal and shear stresses near the free edges can be significantly reduced or even totally eliminated by the proposed technique.
引用
收藏
页码:145 / 165
页数:21
相关论文
共 24 条
[1]  
Pipes, Pagano, Interlaminar stresses in composite laminates under uniform axial extension, J. Comp. Mater., 4, pp. 538-548, (1970)
[2]  
Wang, Crossman, Some new results on edge effect in symmetric composite laminates, J. Comp. Mater., 11, pp. 92-107, (1977)
[3]  
Pagano, Pipes, Some observations on the interlaminar strength of composite laminates, Int. J. Mech. Sci., 15, pp. 679-688, (1973)
[4]  
Hsu, Herakovich, Edge effects in angle-ply composite laminates, Journal of Composite Materials, 11, pp. 422-428, (1977)
[5]  
Wang, Dickson, Interlaminar stresses in symmetric composite laminates, J. Comp. Mater., 12, pp. 390-402, (1978)
[6]  
Spilker, Chou, Edge effects in symmetric composite laminates: importance of satisfying the traction-free-edge condition, J. Comp. Mater., 14, pp. 2-20, (1980)
[7]  
Pagano, Stress fields in composite laminates, Int. J. Solids and Structures, 14, pp. 385-400, (1978)
[8]  
Rybicki, Approximate three-dimensional solutions for symmetric laminates under inplane loading, Journal of Composite Materials, 5, pp. 354-360, (1971)
[9]  
Wang, Choi, Boundary-layer effects in composite laminates Part 1 Free edge stress singularities, Journal of Applied Mechanics, 49, pp. 541-548, (1982)
[10]  
Wang, Choi, Boundary-layer effects in composite laminates Part 2 Free edge stress solutions, Journal of Applied Mechanics, 49, pp. 549-560, (1982)