复杂体系的结构分析和建模研究

根据复杂体系的概念及其所呈现出的多种特性,利用复杂体系的使命分解和复杂体系的元素组成对复杂体系进行综合的结构分析,描述了目标分解、功能分解和行为分解的复杂体系使命目标三阶段分解过程以及系统单元、复合元和体系外部环境的复杂体系三元素结构框架。在此基础上,提出了采用一种“两层四级”的设计思想对复杂体系进行有效的结构建模设计,并针对复杂体系内部的相互位置层次及其功能关联定义了度量实体、层级映射、系统关联性和软构层等相关概念,清晰地阐释了复杂体系结构分析和建模时体系层次映射的实质,从而为复杂体系的效能评估以及体系改进和优化提供一定的理论指导。     

熵理论在装备保障指挥组织结构优化中的应用

把熵理论应用于装备保障指挥组织结构的优化设计,并以某军区装备部机关组织结构为例,从量化的角度比较改革前后组织结构的时效熵和质量熵,得出结论:改革后的军区装备部机关组织结构有序度优于改革前机关组织结构有序度。     

复合固体推进剂颗粒填充模型及其统计特性分析

复合固体推进剂属于高填充比颗粒类复合材料,氧化剂和金属颗粒在基体中的随机分布使其在细观尺度具有非均质的特点。从细观尺度研究固体推进剂燃烧及力学性能时,必须考虑颗粒级配、空间分布和种类等因素的影响。采用分子动力学方法,以硝酸酯增塑聚醚高能复合固体推进剂为研究对象,将固体颗粒模型化为球形,生成其在基体内随机分布的颗粒填充模型。利用Monte-Carlo算法模拟计算颗粒填充模型细观结构的两点概率函数,并研究了颗粒填充体积分数、尺寸与级配等参数对其的影响规律。从统计意义上给出具有各态历经性、统计均匀性和各向同性特点的颗粒填充构型最小周期性代表体元尺寸,可有效减小后续研究的计算量,节约计算成本。所构建的推进剂细观几何构型及对最小周期性代表体元尺寸的计算为后续开展复合固体推进剂细观尺度燃烧、燃面处铝团聚及力学性能数值研究奠定了基础。     

Formation and characterization of core-shell CL-20/TNT composite prepared by spray-drying technique

The core-shell 2,4,6,8,10,12-Hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane/2,4,6-Trinitrotoluene (CL-20/TNT) composite was prepared by spray-drying method in which sensitive high energy explosive (CL-20) was coated with insensitive explosive (TNT). The structure and properties of different formulations of CL-20/TNT composite and CL-20/TNT mixture were characterized by scanning electron microscopy (SEM), Transmission electron microscopy (TEM), Laser particle size analyzer, X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD), differential scanning calorimetry (DSC), impact sensitivity test and detonation performance. The results of SEM, TEM, XPS and XRD show that ϵ-CL-20 particles are coated by TNT. When the ratio of CL-20/TNT is 75/25, core-shell structure is well formed, and thickness of the shell is about 20–30 nm. And the analysis of heat and impact show that with the increase of TNT content, the TNT coating on the core-shell composite material can not only catalyze the thermal decomposition of core material (CL-20), but also greatly reduce the impact sensitivity. Compared with the CL-20/TNT mixture (75/25) at the same ratio, the characteristic drop height of core-shell CL-20/TNT composite (75/25) increased by 47.6% and the TNT coating can accelerate the nuclear decomposition in the CL-20/TNT composites. Therefore, the preparation of the core-shell composites can be regarded as a unique means, by which the composites are characterized by controllable decomposition rate, high energy and excellent mechanical sensitivity and could be applied to propellants and other fields.     

Improving the damage potential of W-Zr reactive structure material under extreme loading condition

Projectiles made of reactive structure materials(RSM)can damage the target with not only kinetic but also chemical energy,but the enhanced damage potential of RSM may become compromised if extreme loading condition disintegrates the projectile before the target is reached.In this work,a ductile coating of Ni was introduced to a tungsten-zirconium(W-Zr)alloy,a typical brittle RSM,to preserve the damage potential of the projectile.Detonation driving tests were carried out with X-ray photography and gun-powder deflagration driving tests were carried out with high-speed photography for the coated and uncoated RSM samples,respectively.The craters on the witness target were analyzed by scanning electron microscopy and X-ray diffraction.The Ni coating was found to effectively preserve the damage potential of the W-Zr alloy under extreme loading conditions,whereas the uncoated sample fractured and ignited before impacting the target in both detonation and deflagration driving.The crack propa-gation between the reactively brittle core and the ductile coating was analyzed based on the crack arrest theory to mechanistically demonstrate how the coating improves the structural integrity and preserves the damage potential of the projectile.Specifically,the Ni coating envelops the W-Zr core until the coated sphere penetrates the target,and the coating is then eroded and worn to release the reactive core for the projectile to damage the target more intensively.     

小波理论在大型空间智能结构振动控制中的应用

采用最优控制理论设计智能结构主动振动控制器,针对大型空间智能结构的低频和密频的特性,基于小波尺度函数变换,设计了智能结构的传感器、致动器;最后通过针对某大型空间智能桁架结构的仿真,表明该控制方法是行之有效的。     

非线性控制在磁悬浮系统中的应用

用滑模变结构控制原理设计磁悬浮系统非线性控制器，并在磁悬浮球装置上进行了试验，结果证实这种控制器具有完全的鲁棒性、良好的参数适应性，设计方法也有广泛的适用性。悬浮系统的刚度有显著的提高。     

“9·11”世贸大楼坍塌原因数值分析

数值分析表明,"9·11"恐怖袭击事件造成纽约世贸大楼的内部竖向承重钢结构的防火保护层在爆炸中严重脱落,火灾高温使钢材强度大幅度降低,导致着火层群柱失稳,上部巨大的冲击荷载把下层柱逐层压渍,引发连续坍塌.最后对超高层建筑的结构设计提出建议.     

金属泡沫复合材料夹芯结构的压痕响应实验

金属泡沫夹芯结构是近年来新出现的一种明显具有结构和功能一体化特点的新型轻质材料,它在临近空间飞行器、航海及汽车等领域有着广阔的应用前景。以以纤维增强复合材料面板、闭孔泡沫铝芯子为特征的复合材料夹芯结构为研究对象,对其在球形压头作用下的压痕响应、损伤模式、变形机制和失效机理进行理论分析和实验研究。研究发现,泡沫铝复合材料夹芯结构的压痕响应是夹芯结构的各个组成部分的响应、相互作用以及压头属性的综合作用结果。泡沫铝复合材料夹芯结构在球压头作用下的损伤模式为基体开裂、纤维断裂、层间分层、泡沫铝的屈服及剪切断裂五种失效模式。     

美军陆战场空域管理体系研究

陆战场空域已经成为一种重要的作战资源,对其进行科学高效的管理十分必要。分析了陆战场空域管理的特点,总结了陆战场空域管理的职能,从条令条例建设、空域管制方法和指挥体系结构等方面对美军陆战场空域管理进行了研究。