Fatigue crack initiation and early growth in the multilayered fibre-metal laminate GLARE 2

被引:0
作者
Vasek, A
Polak, J
Vogelesang, LB
机构
来源
ECF 11 - MECHANISMS AND MECHANICS OF DAMAGE AND FAILURE, VOLS I-III | 1996年
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Results of a recent investigation of fatigue crack initiation and early growth in notched panels of various thickness made of fibre-metal laminate GLARE 2 are presented. Crack initiation life and total life up to the 10 mm crack length are shown. Early microcrack nucleation in inner metal layers and deviation of surface major crack initiation sites from the notch tip are explained in terms of local stress and strain fields in the laminate layers including the residual stress distribution. The decrease of crack growth rate with increasing crack length corresponds to a drop of stress intensity. Effect of the notch factor and the number of lay-ups in the laminate are discussed.
引用
收藏
页码:1685 / 1690
页数:6
相关论文
empty
未找到相关数据