Study on Delamination Behavior and Crack Opening Contour of Advanced Hybrid Laminates during Fatigue Crack Propagation Process
To study crack opening contour and delamination behavior of one kind of advanced hybrid laminates during fatigue crack propagation process,this research accomplished fatigue crack propagation test under R=0.1 for two kinds of saw-cut length and two kinds of stress level,acquired the basic appearance of crack opening contour and delamination,obtained the effect of saw-cut length and stress level on crack opening contour and delamination size.
Fiber metal laminates Advanced hybrid laminates Delamination Fatigue crack propagation Saw-cut
Xiao Huang Jianzhong Liu
Beijing Institute of Aeronautical Materials,Beijing 100095,China
国际会议
北京
英文
1-8
2013-06-16(万方平台首次上网日期,不代表论文的发表时间)