壳装炸药殉爆实验和数值模拟

进行了壳装固黑铝炸药殉爆实验,通过观察残留炸药、壳体和见证板变形,判断被发炸药的爆炸情况,得到了炸药临界殉爆距离。建立了壳装炸药殉爆实验计算模型,采用非线性有限元计算方法,对壳装固黑铝炸药殉爆实验进行了数值模拟。计算中采用预设壳体单元破片方法描述主发炸药壳体破片的形成和破片对被发炸药的撞击起爆,炸药临界殉爆距离的计算结果与实验结果基本一致。主要是主发炸药中部的壳体破片撞击到被发炸药,被发炸药起爆位置也在装药中部。炸药壳体厚度主要影响破片速度和质量、被发炸药的防护性能,从而影响炸药临界殉爆距离。 更多还原     

Some applications of semi-analytical finite element method in static and dynamic analysis of structures

In this paper a kind of semi-analytical finite element method based on the transfer matrix analysis of shells of revolution is briefly formulated. Some recent investigations on its application are presented: (1) a reanalysis algorithm for improving the accuracy of free vibration analysis; (2) a kind of semi-analytical ring element for the stress analysis of a curved pipe of the slender torus shell type.     

非均质变截面杆中弹性波的反射和透射

基于一维弹性波理论，本文对应力波在非均质变截面杆中传播问题进行了一维简单波分析，并把分析结果与二维轴对称有限元分析结果进行了比较，表明一维简单波分析是非常有效和实用的。利用一维简单波分析方法，本文还揭示了应力波在非均质变截面杆中的传播规律，特别对含有内部交界面的非均质变截面杆（带有连接段）进行了一维等效简化分析，研究了连接段对应力波传播的影响。     

航天器火工冲击模拟试验及响应预示方法研究综述

航天器火工冲击力学环境是由星箭分离、部组件展开等工作过程中的火工品起爆引起的作用于结构上的高频、高加速度量级的瞬态冲击响应,能对航天器上含有晶振、脆性材料等的精密电子设备造成致命损伤,是航天器需要经历的最苛刻的力学环境之一。本文中,对国内外航天器火工冲击地面试验方法和环境预示方法做了全面、详细的介绍,总结了这两个方面的研究进展,分析了我国在这两个方面与航天强国的差距。最后,从我国航天工程实际需求出发,提出了今后航天器火工冲击领域应重点开展的研究方向。     

Internal wave reflections and transmissions arising from a non-uniform mesh. Part III: The occurrence of evanescent waves in the Crank-Nicolson linear finite element scheme

The numerical scheme upon which this paper is based is the 1D Crank–Nicolson linear finite element scheme. In Part I of this series it was shown that for a certain range of incident wavelengths impinging on the interface of an expansion in nodal spacing, an evanescent (or spatially damped) wave results in the downstream region. Here in Part III an analysis is carried out to predict the wavelength and the spatial rate of damping for this wave. The results of the analysis are verified quantitatively with seven ‘hot-start’ numerical experiments and qualitatively with seven ‘cold-start’ experiments. Weare has shown that evanescent waves occur whenever the frequency of a disturbance at a boundary exceeds the maximum frequency given by the dispersion relation. In these circumstances the ‘extended dispersion’ relation can be used to determine the rate of spatial decay. In the context of a domain consisting of two regions with different nodal spacings, the use of the group velocity concept shows that evanescent waves have no energy flux associated with them when energy is conserved.     

Three‐dimensional computation for flow‐induced vibrations in in‐line and cross‐flow directions of a circular cylinder

We present numerical results for in‐line and cross‐flow vibrations of a circular cylinder, which is immersed in a uniform flow and is elastically supported by damper‐spring systems to compute vibrations of a rigid cylinder. In the case of a circular cylinder with a low Scruton number, it is well‐known that two types of self‐excited vibrations appear in the in‐line direction in the range of low reduced velocities. On the other hand, a cross‐flow vibration of the circular cylinder can be excited in the range of high reduced velocities. Therefore, we compute the flow‐induced vibrations of the circular cylinder in the wide range of the reduced velocities at low and high Scruton numbers and discuss about excitation mechanisms in the in‐line and cross‐flow directions. Copyright © 2011 John Wiley & Sons, Ltd.