Compression after impact strength of thin laminates with various percentage of 0° plies

被引:5
|
作者
Nettles, Alan Tate [1 ]
Sabo, Stosch [2 ]
机构
[1] NASA MSFC, Marshall Space Flight Ctr, Huntsville, AL 35812 USA
[2] Winona State Univ, Dept Composite Mat Engn, Winona, MN USA
基金
美国国家航空航天局;
关键词
Compression; damage tolerance; impact;
D O I
10.1177/0021998312472219
中图分类号
TB33 [复合材料];
学科分类号
摘要
Conventional wisdom dictates that adding more 0 degrees plies in the load-bearing direction of a laminate will increase its stiffness and strength. While this is true for undamaged laminates, the compression strength of laminates with impact damage may not be as straightforward. In this study, compression after impact strengths of relatively thin laminates with 25%, 33% or 50% of plies aligned in the 0 degrees load-bearing direction were measured for three different damage severity levels. Results show that the increase in compression strength of the laminates with a higher percentage of plies in the 0 degrees direction is lessened as impact damage severity increases indicating that a laminate that is stronger in compression when undamaged may not be stronger in compression when impact damage is accounted for.
引用
收藏
页码:345 / 354
页数:10
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