数值模拟气液针栓式火箭发动机喷雾燃烧对声学激励的响应

为研究气液针栓式火箭发动机的声学振荡特性并为其优化设计提供指导,加工了具有矩形燃烧室的LOX/GCH₄针栓式发动机,采用Euler-Lagrange方法仿真横向速度扰动产生的声学响应,以期在热试前了解声学激励频率对非稳态喷雾燃烧过程的影响。仿真结果表明,采用的横向速度扰动能在燃烧室内产生同频率的一阶横向声学振荡响应。喷雾燃烧对声学激励的响应强弱受扰动频率与燃烧室一阶横向振荡模态固有频率的相对大小影响较大。当扰动频率与该固有频率相等时,压力和燃烧释热随速度扰动出现同相振荡,压力振荡幅值显著增高导致燃烧室前半段的喷雾和火焰同步摆动;同时,燃烧室内存在扩散燃烧变为预混燃烧的趋势,甲烷在更短的距离内燃烧完全且燃烧室温度趋于均匀。     

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。     

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     

并联机构奇异点分析的新方法

根据并联机构位形空间的特点 ,采用微分几何和微分拓扑的方法 ,提出了一种并联机构奇异点的新的分类方法 ,即分为拓扑奇异点 ,参数化奇异点两种类型 ,并把它与现有的几种分类方法进行了比较。     

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.     

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。     

组合末制导律及其仿真研究

传统的比例导引具有很多缺点。第一,在攻击大机动目标时的控制精度差;第二,对导弹的需用过载要求大;第三,增益高的比例导引中任何噪声都会使它的性能大大降低。为了克服上述缺点,提出了一种简单有效的组合末制导规律,即比例加追踪法的组合末制导规律,它继承了纯比例导引所具有的简单、易于实现的优点,同时还可以降低导弹的需用过载,提高导弹的打击精度。经过大量的数字仿真,所提出的组合末制导律,导弹的平均过载和峰值以及终端脱靶量均小于比例导引。