Investigate the effects of magnetic fields on the penetration ability of a shaped charge jet at different standoffs

The influence of a magnetic field on the stability of a shaped charge jet is experimentally investigated at standoffs of 490, 650 and 800 mm. The experimental results without and with the magnetic field are compared in terms of the shaped charge jet form, stability and penetration ability. A theoretical model based on one-dimension fluid dynamics is then developed to assess the depth of penetration of the shaped charge at those three standoffs and magnetic conditions. The results show that the penetration capability can be enhanced in more than 70% by the magnetic field. The theoretical calculations are compared with the experimental results with reasonably good correlation. In addition, the parameters introduced in the theory are discussed together with the experiments at three standoffs studied.     

提高XENIX系统安全可靠性的途径

如何提高ＸＥＮＩＸ系统的安全性、稳定性是很重要的。文中提出的方法经实践证明行之有效,有益于ＸＥＮＩＸ系统的管理和维护。     

具有离散时滞与分时时滞的非自治系统的渐近稳定性

研究了一类具有离散时滞与分布时滞的非自治线性系统的渐近稳定性问题，利用Lyaplunov函数方法和线性矩阵不等式（LMI），得到了系统渐近稳定性的一些充分条件，这些条件能够利用线性矩阵不等式（LMIs）表示，且表达式中含有具有时变时滞与分布时滞项，这样，具有时变时滞与分布时滞的非自治线性系统的稳定性就能够通过Matlab的LIM工具箱进行验证。     

基于Huber权函数的Allan方差非相关差分抗差估计方法

原子钟频率稳定度计算时由于钟差观测异常会导致Allan方差出现较大的估计偏差。本文首先建立了Allan方差的差分估计模型,根据钟差的差分序列统计特性分析了相关差分估计的噪声识别与白化等计算复杂度问题;针对上述难点提出了一种基于Huber权函数的非相关差分抗差估计方法,建立了一种非相关差分序列的构造方法,有效避免了复杂的噪声识别及白化计算,给出了Allan方差的非相关差分抗差估计的推导,并对抗差过程引入的误差累积给出了一种抵消方法;最后给出了完整的抗差估计方案,并利用实测数据进行了实验验证,结果表明本文方法对相位单点跳变、相位阶跃跳变具有显著的抗差能力,抗差估计可使异常引入的相对偏差由近200%降至5%以内。     

When Will Non-Democratic Actors Win a Moral Victory Following Highly Costly Military Defeats?

Following costly military defeats political elites usually attempt to persuade their publics that the battlefield outcome was not a shameful defeat but a ‘moral victory’. Yet, only sometimes their public accepts these claims. The paper tries to explain this variation in the domestic publics' perceptions in the cases of non-democratic entities. It is argued that the key variable that determines actors' success in claiming a moral victory is the existence of certain battlefield elements, or at least symbolic military acts/achievements of the defeated actor which can persuade his public that these battlefield elements existed. Propaganda efforts to misrepresent the battlefield facts can play only a secondary role and only under certain conditions.     

A new experimental way for the monitoring of the real/equivalent in-service-time of double base rocket propellant by coupling VST and PCA

The assessment of the real in-service-time(RIST)and the equivalent in-service-time(EIST)of double base rocket propellants(DBRPs)is of utmost importance for the safe storage and use of weapon systems as well as the efficiency of the accelerated aging plans.In this work,four DBRPs with similar chemical composition and different natural aging have been artificially aged at T = 338.65 K for 4 months with sampling every 30 days.The unaged and artificially aged samples have been investigated by vacuum stability test(VST)at five isothermal temperatures(T = 333.15 K,343.15 K,353.15 K,363.15 K,and 373.15 K).The volume of the evolved gases in VST was found to decrease with natural/artificial aging.Furthermore,the VST data were treated and subjected to principal component analysis(PCA).The results showed excellent discrimination of the DBRP samples according to their stability thermal properties.Most of the variance was described by the first principal component(PC1)whose scores were linearly correlated with the natural aging durations when PCA is applied on VST data obtained at T = 363.15 K.In light of the obtained results,a new experimental way for the estimation of the real/equivalent IST was proposed,which takes into account the impact of the natural aging of the sample.The approach predicts successfully the RIST of two similar DBRPs with a relative deviation of less than 2％.At the specific heating temperature T = 338.65 K,the developed model provides more conceivable EIST values,with asymptotic behavior against artificial aging duration evolution,thus overcoming some shortcomings of the common generalized van't Hoff formula(GvH).     

锥壳稳定方程的一般解

在本文中,用应力函数和中面法向位移表示的锥壳稳定方程被变化成为一对无奇异性的简化方程,然后得出了方程的幂级数形式的一般解。计算结果与已有的实验结果符合良好。计算分析了８种边界情况下边界条件对静水外压临界载荷的影响及解的收敛性。     

潜艇耐压壳体深潜安全性监测技术初探

从设备状态监测诊断技术的一般内容出发,论述了丧失稳定是潜艇耐压壳体在深潜时的主要破坏模式,振动固有频率是表征其安全性储备的特征量。据此提出了安全性监测装置的组成,实艇应用前景及有待研究的问题。     

十二相同步发电机整流系统的数字仿真（Ⅱ）──仿真和试验结果

在“十二相同步发电机整流系统数字仿真研究（Ⅰ）”的基础上,本文详细研究了发电机参数、负载参数、原动机参数、励磁反馈控制参数等对该类系统暂态过程和运行稳定性的影响;较完整、全面地提供了各种运行情况下系统动态和稳态时的数字仿真曲线,从而为设计带整流负载的十二相同步发电机提供参数选择的依据,并能对所设计的该类系统的运行稳定性进行预估。     

导弹气动伺服弹性稳定性分析

导弹气动伺服弹性稳定性分析是导弹受控舵面设计的一个重要问题。针对防空导弹的特点 ,采用气动力导数加下洗修正的非定常气动力方法来计算其气动力。在气动弹性运动方程的建立和气动弹性环节传递函数的确定上 ,采用了传统的主模态法 ,在此基础上 ,利用乃奎斯特法对导弹进行了气动伺服弹性稳定性分析和稳定裕度分析。