摘要
本文对三种环氧树脂基体的碳纤维复合材料含中心圆孔层板的损伤历程进行了实验研究,每种材料分别选用了两种铺层形式;从材料性能的角度讨论了基体和作为一种工艺因素的铺层顺序对层板损伤的影响。
The damage processes of the unnotched and notched compo-site laminates with different matrices and different stacking sequences undertensile loading and tension-compression fatigue loading have been investigatedby using penetrant enhanced x-ray radiography and ultrasonic C-scanningtechnique.The influence of the matrix performance and the stacking sequenceon the damage in the laminates is described in this paper.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1989年第2期1-8,共8页
Chinese Space Science and Technology
关键词
复合材料
层板
损伤
基体
铺层顺序
Graphite-epoxy composite,Damage,Laminated material,Research.
