超空泡运动体圆柱薄壳动力屈曲及可靠性分析

王杰方;安伟光;宋向华

振动与冲击 ›› 2014, Vol. 33 ›› Issue (8) : 22-28.

PDF(1531 KB)
PDF(1531 KB)
振动与冲击 ›› 2014, Vol. 33 ›› Issue (8) : 22-28.
论文

超空泡运动体圆柱薄壳动力屈曲及可靠性分析

  • 王杰方,安伟光,宋向华
作者信息 +

The dynamic buckling and reliability analysis of cylindrical thin shell of supercavitating vehicles

  • WANG Jie-fang, AN Wei-guang, SONG Xiang-hua
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文章历史 +

摘要

首先将超空泡运动体模拟成受动态轴向载荷作用的圆柱薄壳,推导了结构的动力稳定性微分方程和动力不稳定区域,然后考虑动态轴向载荷的随机性,采用有限步长迭代法将给出的动力屈曲失稳的多个安全余量方程线性化,并利用逐步搜索法找出有效的安全余量方程,最后结合逐步等效平面法计算了舱段动力屈曲的可靠性指标。通过算例分别分析了载荷频率、速度和载荷比例系数这三个随机参数的变化对动力屈曲可靠性的影响。计算结果为如何选择载荷频率、速度和载荷比例系数的安全范围提供了理论依据。

Abstract

Firstly, the supercavitating vehicle was simulated by a cylindrical thin shell which was loaded with a axial dynamic load, and the dynamic stability differential equations and the unstable regions of structure were deduced. Secondly, the safety margin equations of dynamic buckling were given and linearized by limit step length iteration method when the randomness of axial load was taken into account, and step-by-step searching method was proposed in search of those effective safety margin equations. Finally, the reliability index of dynamic buckling was calculated with step-by-step equivalent plane method. Through numerical results, the influence of the change of load frequency, velocity and the coefficient of load rate to the dynamic buckling reliability were discussed. The calculate result give a theory foundation to how to choose the safety range of load frequency, velocity and the coefficient of load rate.

关键词

动力屈曲 / 可靠性 / 有限步长迭代法 / 逐步搜索法 / 逐步等效平面法

Key words

Dynamic buckling / Reliability / Limit step length iteration method / Step by step searching method / Step-by-step equivalent plane method

引用本文

导出引用
王杰方;安伟光;宋向华. 超空泡运动体圆柱薄壳动力屈曲及可靠性分析[J]. 振动与冲击, 2014, 33(8): 22-28
WANG Jie-fang;AN Wei-guang;SONG Xiang-hua. The dynamic buckling and reliability analysis of cylindrical thin shell of supercavitating vehicles [J]. Journal of Vibration and Shock, 2014, 33(8): 22-28

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