异构系统一体化仿真中间件系统实现研究

针对异构系统联通的整体化仿真需求,利用Thrift和Zookeeper对一体化仿真中间件系统的组成结构、功能和服务形式等进行了研究,分析了异构系统的升级改造方法,建立了面向服务的异构系统联通仿真的中间件系统架构,实现了跨语言和跨平台的异构应用系统一体化仿真互联互通.系统可扩展、灵活性强,能有效降低异构仿真系统联通升级改造成本,为面向多节点、多任务和高并发的实时在线异构互联一体化仿真提供了可行设计思路.     

Study of high-speed-impact-induced conoidal fracture of Ti alloy layer in composite armor plate composed of Ti-and Al-alloy layers

In order to understand the mechanism of conoidal fracture damage caused by a high-speed fragment-simulating projectile in titanium alloy layer of a composite armor plate composed of titanium- and aluminum-alloy layers, the ballistic interaction process was successfully simulated based on the Tuler-Butcher and GISSMO coupling failure model. The simulated conoidal fracture morphology was in good agreement with the three-dimensional industrial-computed-tomography image. Further, three main damage zones (zones I, II, and III) were identified besides the crater area, which are located respectively near the crater area, at the back of the target plate, and directly below the crater area. Under the high-speed-impact conditions, in zone II, cracks began to form at the end of the period of crack formation in zone I, but crack formation in zone III started before the end of crack formation in zone II. Further, the damage mechanism differed for different stress states. The microcracks in zone I were formed both by void connection and shear deformation. In the formation of zone I, the stress triaxiality ranged from-2.0 to-1.0, and the shear failure mechanism played a dominant role. The microcracks in zone II showed the combined features of shear deformation and void connection, and during the for-mation process, the stress triaxiality was between 0 and 0.5 with a mixed failure mode. Further, the microcracks in zone III showed obvious characteristics of void connection caused by local melting. During the zone III formation, the triaxiality was 1.0-1.9, and the ductile fracture mechanism was dominant, which also reflects the phenomenon of spallation.     

Storage life prediction under pre-strained thermally-accelerated aging of HTPB coating using the change of crosslinking density

In order to predict the storage life of a certain type of HTPB (hydroyl-terminated polybutadiene) coating at 25 C and analyze the influence of pre-strain on the storage life, the accelerated aging tests of HTPB coating at 40 C, 50 C, 60 C, 70 C with the pre-strain of 0%, 3%, 6%, 9%, respectively were carried out. The variation regularity of the change of crosslinking density was analyzed and the aging model of HTPB coating under pre-strained thermally-accelerated aging was proposed. The storage life of HTPB coating at 25 C was estimated by using the Berthelot equation as the end point of the aging life with a 30% decrease in maximum elongation. The results showed that the change of crosslinking density of HTPB coating increased with the increase of aging temperature and aging time, and decreased with the in-crease of pre-strain. Under 0% pre-strain, the relationship between the change of crosslinking density of HTPB coating and the aging time can be described by the logarithmic model with the confidence probability greater than 99%.The stress relaxation phenomenon existed under 3%, 6% and 9% pre-strained aging. The aging model considering chemical aging and pre-strain was established with the confidence probability greater than 90%. The storage life of HTPB coating was 15.2935 years at 25 C under 0% pre-strain, which was reduced by 13.9007%, 75.6949% and 89.7859% under 3%, 6% and 9% pre-strain, respectively. The existence of pre-strain has a serious impact on the storage life of HTPB coating, therefore, the pre-strain should be avoided as much as possible during the actual storage.     

中国近海海空联合作战环境风险综合区划方法

针对中国近海海空联合作战环境风险区划问题,选取水面舰艇航行、舰载机飞行、海上人员训练等作战样式,大风、大浪、低云低能见度、湿热、风寒等环境要素,高值频率、概率极值、平均强度、气候趋势等指标,利用层次分析法和互反判断矩阵建立四层评价体系并进行区划.该方法可根据装备设计及环境适应标准对各指标进行影响排序,能有效区分不同季节和动力机制的环境要素差异、综合考虑不同类型风险影响.区划结果证明,海空联合作战环境风险由各兵种作战风险综合决定,主要受秋冬季盛行大风、夏秋季热带气旋、春夏季低能见度、冬春夏季低云、夏季湿热指数、冬季风寒指数等影响.     

超音速等离子喷涂WC-Co涂层性能研究

用超音速等离子喷涂(HEPJet)和2种进口高速氧燃气火焰喷涂设备 (HVOF:JP-5000和DJ-2700)制备WC-Co涂层,进行了孔隙率、显微硬度、结合强度及30°和90°攻角的冲蚀磨损对比试验,用XRD分析了粉末和涂层的相结构,用 SEM分析了粉末和涂层的表面和断面形貌。结果表明3种工艺制备的WC-Co涂层与粉末的相结构类似,均无明显氧化、失碳;超音速等离子喷涂WC-Co涂层综合性能与JP-5000相当,要优于DJ-2700。     

陆军防空兵体制编制信息化评估模型研究

针对信息化条件下陆军防空兵体制编制的主要特点和发展趋势,研究了如何定量评估其信息化程度问题。运用模糊综合评判法和综合评分分析法建立了防空兵体制编制信息化评估模型。并以某防空旅为例进行了实例测评,基本上反映了该旅体制编制信息化建设的真实水平,证明建立的模型是可行和正确的。而且,通过对不同元素测评结果的对比分析,可以清楚地看出测评对象体制编制各元素信息化建设的发展态势,找出下一步建设的努力方向。     

单[6-脱氧（1，10癸二硫醇）巯基]β-环糊精的合成方法研究

制备合成单[6-脱氧（1,10癸二硫醇）巯基]β-环糊精,结合产物的。^1H NMR,^13C HMR分析,推测了可能的反应机理,初步讨论了其在制备传感器敏感膜材料方面的应用前景。     

改进的接触算法及其在光滑粒子流体动力学中的应用

采用以黎曼解描述粒子间相互作用的接触算法,模拟一维情况下包含间断的流场。在弱间断的条件下,采用弱波近似的黎曼解来描述粒子间的相互作用;在强间断的条件下,则引入非迭代黎曼解来描述粒子间的相互作用。并引入Taylor展开思想,提高了接触算法在自由边界的计算精度。该算法无需引入人为粘性,程序结构简洁。数值计算表明,改进后的接触算法能很好地描述强间断,并有效改善了原始接触算法在自由面的计算缺陷。     

基于生物视觉原理的图像结构信息变化检测方法

为克服多时相遥感图像变化检测中照度差异和配准误差的影响,采用边缘结构信息进行变化检测。利用多方向Gabor函数从图像梯度强度图中提取边缘结构信息,称之为边缘标记(Edge Tag,ET),通过比较多时相遥感图像中ET的互相关系数实现变化检测。为减小差异较小的边缘对检测结果的影响,在相关系数的计算中引入抑制因子。仿真图像和真实图像的实验结果表明,该方法能克服图像照度差异和配准误差对变化检测的影响,取得了较好的检测效果。     

利用混合编程改善SMP机群上并行矩阵乘法的性能

针对SMP机群,探讨了分别利用单机优化、OpenMP与MPI从指令级、共享存储级与分布主存级三个层次上改善矩阵并行乘Fox算法性能的方法。并通过调用数学函数库与混合编程的方式,在深腾6800上进行了实验,取得了相当满意的数值效果。