Opening behavior of PELE perforation on reinforced concrete target

Impact velocity (v0), target strength (fc) and target thickness (hc) are important factors affecting opening damage ((D)) of PELE penetration into RC target. In this paper, based on the three influence factors of v0, fc and hc, experimental and numerical simulation studies on PELE penetration into RC target were carried out. The study results show that: (1) Since interaction force (or penetration resistance) between pro-jectile and target is positively correlated with v0 and fc, with the increase of v0 and fc, deformation mode of jacket is changed from small bending deformation to large bending deformation and then to curling deformation. Therefore, the variation of jacket deformation mode causes opening diameter of RC target to increase first and then to decrease. It is found that the two factors approximately satisfy a quadratic function relationship, respectively. (2) For PELE projectile penetrating RC targets with thickness of 80—400 mm, the opening diameter of six sets of RC targets grows from 240 to 500 mm, and hc with (D) approximately satisfy a linear relationship. (3) Based on the above study results, the relationship be-tween two dimensionless parameters (I= (mv20/d31fc) and H= hc/l ) and dimensionless opening diameter ((D)/d1) was determined. Combined with the results of previous research, a dimensionless opening diameter model (D)/d1=f1(Q,G,I)f2(H) was established. By tests verified, the test results are all within ±10％error of the theoretical model, which verifies the accuracy of the model.     

Dynamic necking of a near α titanium alloy at high strain rates:Experiments and modelling

The tensile behaviour of near α Ti3Al2.5 V alloy, conceived for applications in aerospace and automotive engineering, is characterized from quasi-static to high strain rates. The material is found to present noticeable strain rate sensitivity. The dynamic true strain rate in the necking cross-section reaches values up to ten times higher than the nominal strain rate. It is also observed that beyond necking the dynamic true stress-strain curves present limited rate dependence. The experimental results at different strain rates are used to determine a suitable constitutive model for finite element simulations of the dynamic tensile tests. The model predicts the experimentally macroscopic force-time response, true stress-strain response and effective strain rate evolution with good agreement.     

Fabrication and characterization of Al-CuO nanocomposites prepared by sol-gel method

In this study, Al-CuO nanocomposites were fabricated by sol-gel method. As a contrast, the thermite was prepared by physical mixing at the equivalence ratio of 0.5, 1, 2, respectively. The intermediates and samples as prepared were characterized by SEM and XRD. The exothermic properties of the two samples prepared at different equivalence ratios were tested and the reaction products were characterized by XRD. The SEM results show that the sample prepared by the sol-gel method demonstrates a micron-sized agglomerated sphere formed by a mutual wrapping of Al NPs and CuO NPs, and the particles are evenly distributed in the agglomerate. In addition, when the content of Al powder is seriously insufficient, the heat release of the sample prepared by physical mixing is 1.6 times that of by sol-gel method. With the increase of Al powder content, the exothermic properties of Al/CuO NPs prepared by sol-gel method began to increase significantly compared with physical mixing and the difference is 1.5 times when the equivalence ratio increases to 2. It can be concluded that the reason for this result may be attributed to the different mass transfer modes of components due to the different morphologies of samples.     

Damage to aircraft composite structures caused by directed energy system: A literature review

This paper presents a comprehensive review of the research studies on direct energy system effect on aircraft composite structures to develop a good understanding of state-of-the-art research and devel-opment in this area. The review begins with the application of composite materials in the aircraft structures and highlights their particular areas of application and limitations. An overview of directed energy system is given. Some of the commonly used systems in this category are discussed and the working principles of laser energy systems are described. The experimental and numerical studies re-ported regarding the aircraft composite structures subject to the effect of directed energy systems, especially the laser systems are reviewed in detail. In particularly, the general effects of laser systems and the relevant damage mechanisms against the composite structures are reported. The review draws attention to the recent research and findings in this field and is expected to guide engineers/researchers in future theoretical, numerical, and experimental studies.     

Numerical research on adverse effect of muzzle flow formed by muzzle brake considering secondary combustion

The simulation of the artillery interior and intermediate ballistics problem is performed to investigate the influence of a gas dynamics device, muzzle brake, on the muzzle hazard phenomena, such as flash and blast waves. The correlation of the chemical reactions with the characteristics of the muzzle flow field is analyzed by the simulation for a further understanding of the secondary combustion phenom-enon of the muzzle flow. The novel structure of muzzle flow caused by the muzzle brake is presented by the simultaneous solution of the interior ballistics model and multi-species Navier-Stokes equations in order to analyze the influence of the muzzle brake structure on the chemical reactions. The secondary combustion of the muzzle flow due to the oxygen-supplement chemical reactions is obtained by the chemical reaction kinetic model. The interaction of the blast waves released from the muzzle brake is illustrated in detail and the mechanism of the formation of muzzle flash is analyzed. This research provides a reference for the studies on the suppression of the muzzle flash.     

RPL路由协议中基于投票法的黑洞攻击检测算法

物联网容易遭受多类拒绝服务攻击,其中黑洞攻击是最严重的攻击之一.为此,提出基于投票法的黑洞攻击检测算法(Voting Method-based Blackhole Attack Detection,VMBAD).通过VMBAD算法检测RPL协议上的黑洞攻击.先通过过滤器构建嫌疑节点,再验证嫌疑节点的行为,各节点作出自己的决策意见,并传输到边界路由(Bor-der Router,BR).接收后,BR利用投票机制融合各节点的决策意见,进行最终的决策,进而判断节点是否为黑洞攻击节点.一旦认定为黑洞攻击,就将黑洞攻击节点与网络隔离,使其不参与RPL路由.仿真结果表明,VMBAD算法能够有效地检测黑洞攻击节点,并且通过排除攻击节点,提高了数据包传递率.     

废放射源处置方法研究

针对防化部（分）队应用放射源与含源装备仪器过程中产生大量废放射源的问题,根据国家和军队相关法规和标准,提出关于废放射源分类、收集、包装、运输、建库、储存和最终处置的贴近部队实际的处置方法要求．     

次氯酸钙乳液消毒剂模拟剂的研究

研究了一种次氯酸钙乳液消毒剂的模拟剂,以及一些影响稳定性因素．该模拟剂是以氢氧化钙为分散相,水为分散介质,表面活性剂和无机盐为稳定剂组成．实验结果表明,该模拟剂具有与次氨酸钙消毒乳液相同的物理性能,并且无污染,可用于教育、作训之中．     

烟幕弹弹丸可视化设计系统建模方法研究

介绍了对烟幕弹弹丸进行可视化设计可行性的研究,以某型号烟幕弹弹丸为实例阐述了参数化模型的建立方法及特征数自动计算的实现,并对该可视化设计程序进行了验证。     

CR-39中子探测效率的模拟研究

利用蒙特卡罗（MC）方法计算了CR-39探测器对中子的探测效率,并与文献结果进行比较,得出了一致的结论;同时以^252Cf自发裂变源为模拟中子源,通过MCNP程序计算,得出了中子探测效率随CR-39探测器厚度变化的曲线。