Dynamic buckling and reliability analysis of a cylindrical thin shell for supercavitating vehicles

被引:0
作者
机构
[1] Department of Aerospace Engineering, Harbin Engineering University
来源
Wang, J.-F. | 1600年 / Chinese Vibration Engineering Society卷 / 33期
关键词
Dynamic buckling; Limited step length iteration method; Reliability; Step-by-step equivalent plane method; Step-by-step searching method;
D O I
10.13465/j.cnki.jvs.2014.08.005
中图分类号
学科分类号
摘要
Firstly, a supercavitating vehicle was modeled as a cylindrical thin shell loaded with a axial dynamic load. The dynamic stability differential equations and the unstable regions of the shell were deduced. Secondly, the safety margin equations for its dynamic buckling were given and linearized with the limited step length iteration method considering the randomness of axial load. Then, the step-by-step searching method was proposed to search those effective safety margin equations. Finally, the reliability index of the dynamic buckling was calculated with the step-by-step equivalent plane method. Through numerical examples, the influences of change of load frequency, velocity and proportional coefficient of load on the dynamic buckling reliability were analyzed, respectively. The calculation results provided a theoretical basis for choosing the safety range of load frequency, velocity and proportional coefficient of load.
引用
收藏
页码:22 / 28
页数:6
相关论文
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