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Failure analysis of a frangible composite cover: A transient-dynamics study
Cai, Deng'an; Zhou, Guangming; Qian, Yuan; Silberschmidt, Vadim V.
刊名JOURNAL OF COMPOSITE MATERIALS
2017
卷号51期号:18页码:2607-2617
英文摘要A transient-dynamics model based on the approximate Riemann algorithm is proposed for the failure analysis of a frangible composite canister cover. The frangible cover, manufactured with a traditional manual lay-up method, is designed to conduct a simulated missile launch test using a specially developed test device. Deformation of the cover's centre is determined using a transient-dynamics finite element model; failure pressure for the frangible cover is obtained based on a failure criterion and compared with simulated experimental results. Weak-zone position of the frangible cover has a significant effect on failure pressure compared to that of deformation of the cover's centre. With the same structure of the weak-zone, an increase in its height can first raise and then reduce the level of failure pressure of the frangible cover. Close agreements between the experimental and numerical results are observed.
语种英语
内容类型期刊论文
源URL[http://libir.pmo.ac.cn/handle/332002/17353]  
专题中国科学院紫金山天文台
推荐引用方式
GB/T 7714
Cai, Deng'an,Zhou, Guangming,Qian, Yuan,et al. Failure analysis of a frangible composite cover: A transient-dynamics study[J]. JOURNAL OF COMPOSITE MATERIALS,2017,51(18):2607-2617.
APA Cai, Deng'an,Zhou, Guangming,Qian, Yuan,&Silberschmidt, Vadim V..(2017).Failure analysis of a frangible composite cover: A transient-dynamics study.JOURNAL OF COMPOSITE MATERIALS,51(18),2607-2617.
MLA Cai, Deng'an,et al."Failure analysis of a frangible composite cover: A transient-dynamics study".JOURNAL OF COMPOSITE MATERIALS 51.18(2017):2607-2617.
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