Effects of nano-sized aluminum on detonation characteristics and metal acceleration for RDX-based aluminized explosive

Nano-sized aluminum(Nano-Al)powders hold promise in enhancing the total energy of explosives and the metal acceleration ability at the same time.However,the near-detonation zone effects of reaction between Nano-Al with detonation products remain unclear.In this study,the overall reaction process of 170 nm Al with RDX explosive and its effect on detonation characteristics,detonation reaction zone,and the metal acceleration ability were comprehensively investigated through a variety of experiments such as the detonation velocity test,detonation pressure test,explosive/window interface velocity test and confined plate push test using high-resolution laser interferometry.Lithium fluoride(LiF),which has an inert behavior during the explosion,was used as a control to compare the contribution of the reaction of aluminum.A thermochemical approach that took into account the reactivity of aluminum and ensuing detonation products was adopted to calculate the additional energy release by afterburn.Combining the numerical simulations based on the calculated afterburn energy and experimental results,the param-eters in the detonation equation of state describing the Nano-Al reaction characteristics were calibrated.This study found that when the 170 nm Al content is from 0％to 15％,every 5％increase of aluminum resulted in about a 1.3％decrease in detonation velocity.Manganin pressure gauge measurement showed no significant enhancement in detonation pressure.The detonation reaction time and reaction zone length of RDX/Al/wax/80/15/5 explosive is 64 ns and 0.47 mm,which is respectively 14％and 8％higher than that of RDX/wax/95/5 explosive(57 ns and 0.39 mm).Explosive/window interface velocity curves show that 170 nm Al mainly reacted with the RDX detonation products after the detonation front.For the recording time of about 10 μs throughout the plate push test duration,the maximum plate velocity and plate acceleration time accelerated by RDX/Al/wax/80/15/5 explosive is 12％and 2.9 μs higher than that of RDX/LiF/wax/80/15/5,respectively,indicating that the aluminum reaction energy significantly increased the metal acceleration time and ability of the explosive.Numerical simulations with JWLM explosive equation of state show that when the detonation products expanded to 2 times the initial volume,over 80％of the aluminum had reacted,implying very high reactivity.These results are significant in attaining a clear understanding of the reaction mechanism of Nano-Al in the development of aluminized explosives.     

2K-H 行星传动的极限传动比

在行星轮系机构综合中,研究行星轮数目与极限传动比的关系有着极其重要的意义。本文根据２Ｋ─Ｈ行星轮系机构的同心条件、安装条件和邻接条件,采用统一的符号,对满足上述条件的所有（六种）２Ｋ─Ｈ行星轮系机构,导出了行星轮个数与极限传动比的统一关系式,得到了所有２Ｋ─Ｈ行星轮系机构的极限传动比计算公式,为２Ｋ─Ｈ行星轮系机构的综合提供了理论根据。     

航空燃料水反应试验条件对试验结果的影响

航空燃料水反应试验是检测喷气燃料和航空汽油洁净性指标的一个重要方法,该方法的试验结果受试验条件影响.探讨了试验条件对试验结果的影响,通过考察摇动速率和摇动幅度,提出了优化摇动速率和摇动幅度的试验控制条件.在摇动时间为2min、摇动速率为150次/min、摇动幅度控制在185 mm、静置时间为5 min进行试验时,其试验结果均呈现很好的重复性和再现性,较好地消除了方法中试验条件控制对试验结果的影响.     

Group support for political violence: The role of emotions and expressive choice in creating conflict or providing peace

This paper provides a rationale for group support for political violence which does not provide a material benefit. Rabin’s (1993) theory of fairness is adopted to demonstrate that although group violence may not be a Nash equilibrium it may be a fairness equilibrium in a game containing psychological payoffs. For this to happen the material stakes must be perceived as low and psychological payoffs are expressive. Although the material stakes are actually high, members of each group may choose expressively to support the use of violence because the probability of being decisive is low. The paper also considers the possibility of peace emerging as a fairness equilibrium. This can only happen if each group perceives the other as making some sacrifice in choosing peace.     

Purchase and retrieval competition for seasonal produce

We study the competition problem of purchase and multiretrieval of perishable seasonal produce, where wholesalers purchase and stock their products in the first period, and then retrieve and sell them in subsequent periods. We first consider the duopoly case and assume that the prices are exogenous and fluctuate. In each period, after the price realization, the wholesalers retrieve some stock from their warehouses to satisfy their demands. One wholesaler's unsatisfied customers can switch to another and be satisfied by its left retrieved products. Any unsold retrieved stock has no salvage value and any unsatisfied demand is lost. The unretrieved stock is carried to the next period at a perishable rate. The wholesalers compete for the substitute demand by determining their own purchase and retrieval quantities. We show the existence and uniqueness of a pure-strategy Nash equilibrium, and that the Nash equilibrium strategy has the simple “sell-down-to” structure. We also consider the general N-person game and show the existence of the Nash equilibrium, and characterize the structure of the equilibrium strategy for the symmetric case. In addition, we consider the case with endogenous prices, and show that the problem reduces to a repeated newsvendor game with price and inventory competition. We derive the conditions under which a unique Nash equilibrium exists and characterize the equilibrium strategy. Finally, we conduct numerical studies to examine the impacts of the model parameters on the equilibrium outcomes and to generate managerial insights.     

状态空间表达下控制系统的稳态误差

经典控制理论对系统稳态误差的讨论从传递函数入手,重点是对系统开环传递函数的研究,当系统的输入是任意函数时,引入动态误差系数方法来研究稳态误差,但是当输入具有高阶导数时,动态误差系数将很难得到.现代控制理论中的状态空间表达下求系统的稳态误差很好地解决了这个问题.利用矩阵之间的运算来表示动态误差系数,并且可以得到任意输入下的稳态误差值,在线性定常系统下的推导结果还可以适用于线性时变系统,具有一定的普遍性.     

模拟体系对抗价值链的网络同步模型

描述战斗毁伤"规模效应"的Lanchester模型默认作战体系内部是"完美的"。本文扬弃此假设,首次从作战体系内部"共识"涌现的视角提出了一个模拟体系对抗价值链的网络"同步效应"模型,研究了战场变化、个体/群体认知、自同步与对抗均衡等概念的网络拓扑和权值演化形式,并发现在对抗均衡条件下无标度网络具有"同步脆弱性"。     

PHM在空空导弹勤务保障中的应用

简要介绍了PHM概念和国内外研究现状,参照OSA-CBM模型,提出了空空导弹PHM系统结构,并阐述了各个模块的功能作用。分析了PHM技术应用于空空导弹贮存的效益和影响可靠性的因素,确定了监测参数,根据尺寸、成本等提出传感器选型要求,构建空空导弹包装箱状态监控系统。通过市场调查,确定了可用于状态监控系统的传感器类型,对未来应用于导弹内部的传感器系统提出了期待。     

基于卫星数据链路的飞机主动维修保障系统

基于北斗卫星数据链路,采用了"空-地"两级数据处理方式进行飞行参数在线判读、主动维修保障及安全监控系统的实时处理。分析了主动维修保障及飞机实时状态监控、北斗短报文系统的基本情况,并着重介绍了系统的总体结构和优势,以及包括机载部分、地面处理系统和北斗卫星数传装置三部分的工作原理和设备构成。     

主元分析法和模糊积分的航空发动机气路状态监测

航空发动机是一个大系统,由于结构复杂、工作条件恶劣等因素影响,对其进行有效地健康状态监测成为航空领域长期难以解决的关键技术之一。为有效监测航空发动机健康状态,以航空发动机气路系统为例,提出一种基于主元分析和模糊积分的航空发动机状态监测方法。首先,利用主元分析法提取发动机状态样本集的主元,对样本数据进行降维,实现样本的最优压缩。其次,利用BP神经网络和Elman神经网络对发动机状态信息的特征向量进行初步状态监测。最后,利用模糊积分对采用两种神经网络的初步监测结果进行决策层融合,从而有效地实现对航空发动机气路系统的状态监测。通过某型真实航空发动机验证表明,所提出基于主元分析和模糊积分的状态监测方法,能有效提高监测的准确度,满足航空发动机状态监测的实时性要求,具有良好的工程应用价值。