Compression Failure Analysis of Adhesively Stiffened Composite Panels
Experimental and numerical investigations of adhesively stiffened composite panels were performed to discuss the load-carrying capacity of different design at stiffener run-out.The compression experiment revealed that the failure was initiated at the edge of the run-out and propagated across the skin-stiffener interface.A fracture mechanical approach to utilize cohesive finite element was adopted in the numerical analysis of these specimens.It was shown that the finite element analysis using solid element and cohesive element was able to qualitatively predict the crack growth characteristics for each specimen.
stiffened composite panels stiffener run-out compression experiment cohesive finite element crack growth
Chunlan Zhang Purong Jia Liang Li Guiqiong Jiao
Engineering Mechanics Department,Northwestern Polytechnical University,710129,Xian
国际会议
西安
英文
322-325
2012-06-12(万方平台首次上网日期,不代表论文的发表时间)