Shaped charge penetration into high- and ultrahigh-strength Steel–Fiber reactive powder concrete targets

Experiments on shaped charge penetration into high and ultrahigh strength steel-fiber reactive powder concrete (RPC) targets were performed in this paper. Results show that the variation of penetration depth and crater diameter with concrete strength is different from that of shaped charge penetration into normal strength concrete (NSC). The crater diameter of RPC is smaller than that of NSC penetrated by the shaped charge. The jet particles are strongly disturbed and hardly reach the crater bottom because they pass through the narrow channel formed by jet penetration into the RPC. The effects of radial drift velocity and gap effects of jet particles for a shaped charge penetration into RPC target are discussed. Moreover, a theoretical model is presented to describe the penetration of shaped charge into RPC target. As the concrete strength increases, the penetration resistance increases and the entrance crater diameter decreases. Given the drift velocity and narrow crater channel, the low-velocity jet particles can hardly reach the crater bottom to increase the penetration depth. Moreover, the narrow channel has a stronger interference to the jet particles with increasing concrete strength; hence, the gap effects must be considered. The drift velocity and gap effects, which are the same as penetration resistance, also have significant effects during the process of shaped charge penetration into ultrahigh-strength concrete. The crater profiles are calculated through a theoretical model, and the results are in good agreement with the experiments.     

旋转永磁式机械天线的研究与实现

为实现低频电磁发信系统的小型化和低功耗,对基于旋转永磁体的机械天线,即利用永磁体机械旋转直接激励电磁波的新型低频电磁发信技术进行了理论研究与工程实践。提出基于钕铁硼永磁体和永磁同步电机的旋转永磁式机械天线技术方案及其信息加载方法,构建基于电-机械-电磁能量转换的系统模型,对其辐射效率和辐射功率进行初步分析,研究旋转永磁体在不同无限均匀介质中产生时变磁场的分布与衰减特性,研制了原理样机,并对其近区磁场和2FSK信号的加载特性进行了实验测试,验证了该方案的可行性和有效性。     

机动管线河流水面铺设牵引力分析与计算

机动管线在穿越河流时常采用水面浮运的方式铺设到对岸,铺设过程中,准确计算管线所受拉力是可靠地设计穿越装备、管线安全施工及运行的关键。建立了水面浮运的数学模型,得出了受力面积的选取方法,利用积分法导出了管线两端拉力的计算公式,指出了影响拉力的因素。采用3种流速方式分别计算出管线两端的拉力并进行了比较,采用符合实际情况的水面流速函数计算出的结果比较合适,对铺设设备的选取提供了理论支撑,对管线铺设有一定的参考价值。     

超声冲击处理改善22SiMn2TiB装甲钢抗应力腐蚀性能研究

采用超声冲击处理工艺对22SiMn2TiB装甲钢试样进行了表面冲击强化,采用四点弯曲加载装置将处理和未处理的试样在3.5%NaCl溶液中进行了150 d的应力腐蚀试验。用X射线应力测定仪测定了应力腐蚀试验前试样表面的残余应力,用扫描电镜和透射电镜观察了处理后试样的断面组织。分析了超声冲击处理引起的残余应力和断面组织变化对改善装甲钢抗应力腐蚀性能的作用。结果表明,超声冲击处理引入的残余压应力和表层晶粒细化可以大大提高22SiMn2TiB装甲钢的抗应力腐蚀性能。     

导弹制导控制与目标杀伤

采用协方差分析描述函数技术 (CADFT)对寻的导弹的制导精度进行了研究 ,提出了空气动力控制、直接侧向力控制的寻的导弹飞行末端的制导精度的一种新的解析模型 ,并研究了导弹直接碰撞杀伤目标的必要条件 ,该理论研究成果具有简单、实用、精度高的特点 ,为寻的导弹制导控制特性研究和揭示寻的理论普遍规律提供了一种新途径     

理想气体绝热过程的微观实质

从分子动理论出发,建立理想气体绝热过程的微观模型,用麦克斯韦速度分布函数导出其过程方程.     

空气阻力对排球正面上手发球水平方向飞行距离的影响实验分析

该文以体院排球普修课男生为对象,通过高速摄影方法,对"空气阻力对正面上手发球水平方向飞行距离的影响"这一问题进行了实验研究.初步揭示了当击球高度,击球角度和击球初速度等条件一定的情况下同,正面上手发球在水平方向飞行的理论距离与实际距离的差值规律.     

基于速度障碍的无人机避免机动障碍物问题

针对无人机避免机动障碍物的问题,应用速度障碍法,在充分考虑障碍物可达范围和无人机最大机动能力的基础上,将问题空间转换到了速度空间,然后以速度障碍的边界条件替代速度障碍的整体范围约束,这样得到了速度障碍的简单表达形式。最后结合最优控制,在速度空间解决了无人机避免障碍物的问题,并直接求解出了合适的速度输出。仿真结果表明方法切实可行。     

917低磁钢与铝合金爆炸焊接复合实验研究

采用异种金属爆炸焊接复合技术 ,研制了 91 7低磁钢与LF5、LF2 1、LF1 1等铝合金的爆炸焊接复合板 ,并对该铝—钢复合板力学性能进行了实验研究 ,对复合界面进行了金相分析 .实验结果表明 ,该铝—钢复合板复合界面物理结合良好 ,其抗剪和抗弯强度满足实船使用要求     

Characteristics structure analysis on debris cloud in the hypervelocity impact of disk projectile on thin plate

In this paper, the gauge points setting is introduced in the SPH simulation to analyze the debris cloud structure generated by the hypervelocity impact of disk projectile on thin plate. Compared with the experiments, more detailed information of the debris cloud structure can be classified from the numerical simulation. However, due to the solitary dispersion and overlap display of the particles in the SPH simulation, accurate comparison between numerical and experimental results is difficult to be performed. To track the velocity and spatial distribution of the particles in the debris cloud induced from disk and plate, gauge points are locally set in the single-layer profile in the SPH model. By analyzing the gauge points’ spatial coordinate and velocity, the location and velocity of characteristic points in the debris cloud are determined. The boundary of debris cloud is achieved, as well as the fragments distribution outside the main structure of debris cloud.