Simulation of the plasticizing behavior of composite modified double-base (CMDB) propellant in grooved calendar based on adaptive grid technology

The frequent occurrence of safety accidents during the calendering process is caused by the flammable and explosive properties of composite modified double-base (CMDB) propellant. Optimization of process parameters with the aid of fluid simulation technology could effectively ensure the safety of the calendering process. To improve the accuracy of the simulation results, material parameters and model structure were corrected based on actual conditions, and adaptive grid technology was applied in the local mesh refinement. In addition, the rheological behavior, motion trajectories and heat transfer mechanisms of CMDB propellant slurry were studied with different gaps, rotational rates and temperatures of two rollers. The results indicated that the refined mesh could significantly improve the contour clarity of boundaries and simulate the characteristics of CMDB propellant slurry reflux movement caused by the convergent flow near the outlet. Compared with the gap, the increased rotational rate of roller could promote the reflux movement and intensify the shear flow of slurry inside the flow region by viscous shear dragging. Meanwhile, under the synergistic effect of contact heat transfer as well as convective heat exchange, heat accumulated near the outlet and diffused along the reflux movement, which led to the countercurrent heat dissipation behavior of CMDB propellant slurry. The plasticizing mechanism of slurry and the safety of calendering under different conditions were explored, which provided theoretical guidance and reference data for the optimization of calendering process conditions. Based on the simulation results, the safety of the CMDB propellant calendering process could be significantly improved with a few tests conducted during a short research and development cycle.     

Mitigation of the blast load effects on a building structure using newly composite structural configurations

In this study, a nonlinear three-dimensional hydrocode numerical simulation was carried out using AUTODYN-3D to investigate the effect of blasting of a high explosive material (TNT) against several configurations of the composite structure. Several numerical models were carried out to study the effect of varying the thickness of the walls and the effect of adding an air layer or aluminum foam layer inside two layers of concrete in mitigating the effect of blast waves on the structure walls. The results showed that increasing the thickness of walls has a good effect on mitigating the effect of blast waves. When a layer of air was added, the effect of blast waves was exaggerated, while when a layer of aluminum foam was added the blast wave effects were mitigated with a reasonable percentage.     

面向两类典型分析仿真的多样本任务调度工具的设计

当在多台计算机上调度很多样本并行运行时,采用手工操作效率低且极易出错。设计一个自动化的任务分发与调度工具可以有效地提高仿真运行效率。蒙特卡罗仿真和粒子群优化算法仿真是两类典型的分析仿真,介绍了面向这两类仿真的多样本任务调度工具的实现原理和关键技术,这些方法具有很好的通用性和可扩展性,可以广泛应用于解决各类仿真任务的自动分发与调度问题。     

基于随机有限集理论的多传感器目标联合检测跟踪算法

针对杂波环境中的目标检测跟踪问题,提出一种基于随机有限集理论的多传感器目标联合检测跟踪算法。算法将目标状态和量测描述为随机集合,建立考虑目标出现、目标保持、目标消失等情况的目标状态随机有限集模型,以及考虑漏检和虚警的多传感器量测随机有限集模型。将目标的联合检测跟踪问题构建为目标状态集合的贝叶斯最优估计问题,并基于随机有限集理论对该贝叶斯估计算法的递推表达式进行严格理论推导。采用序贯蒙特卡罗技术实现算法的递推滤波。仿真结果验证了该算法的有效性以及算法相对于传统基于数据关联算法的性能优势。     

等离子体粒子模拟中的电磁场边界条件

针对等离子体粒子模拟中电磁场边界条件的选取问题 ,对简单吸收边界条件、Lindman边界条件、超吸收边界条件等进行了详细的讨论。结果表明 ,简单吸收边界条件计算量最小、误差最大 ,超吸收边界条件计算量最大、误差最小 ,Lindman边界条件误差较小且其反射系数对入射角的依赖性不大     

平面光波导的数值传递函数方法

把数值传递函数方法应用于对平面光波导的分析。本方法从光波导的标量变分关系出发 ,通过状态方程对问题求解计算。文中引入了传递函数无穷单元的概念 ,使得本方法在处理近截止区域的问题时更加合理 ,计算量更小。文后给出了本文方法的应用和算例 ,与多种方法进行了比较 ,表明本文方法在处理折射率均匀分布和渐变分布波导时都有着特有的优势。     

磁通门探测器的数值分析与仿真

给出了磁通门探测器的数学模型及其数值分析和计算机仿真的方法,并通过实例计算和模拟探测器内部各种物理量的波形、量值和相互关系,解决了电压源激励和非正弦波激励在传统分析计算中存在的难题,最后针对第Ⅱ类磁芯进行了分析.     

平板翼流体动力边界积分多重网格计算

讨论了平板翼流体动力边界积分法多重网格计算模型,给出了残差计算格式和函数修正值计算公式,推导出与步长无关的环量多重网格计算公式.计算结果表明,利用多重网格方法加快了收敛速度,其数值计算的流体动力与试验值吻合.     

德文版液压系统模拟仿真软件的汉化方法

介绍了德文版的 Fluid SIM-H液压系统模拟仿真软件 ,并介绍了应用 Exe Scope、Help Deco、Help Work和 Create Install等工具软件对德文版软件进行汉化的基本方法     

地面防空作战信息对抗模型研究及仿真

在地面防空作战中,地空导弹和空中目标的对抗是一个动态的对抗过程。通过把模型分为自身状态和对对方的估计状态,建立了防空作战对抗模型,分析了导弹追击和目标逃避时的控制输入的选择原则。通过仿真,得到了较好的结论,体现了导弹和目标之间的对抗性,对进一步研究地面防空系统对抗性建模方法具有重要意义。