Design and analysis of a scheme for the naval gun test shell entering the bore

The test shell without projectile belt is widely used in the teaching, inspection and maintenance of modern automatic naval guns. In order to ensure the normal work of each mechanism, it is very important to design the buffer and limit of the test shell during the process of entering the bore. Taking a certain type of medium caliber naval gun as the research object, the design of colloidal fluid damper and cartridge lock was proposed to ensure the reliability of entering the bore and closing the breechblock. By combining the simulation methods of computational fluid dynamics (CFD) and multibody system dy-namic (MBD), it was analyzed whether the structural design can meet the engineering requirements. The research results show that the colloidal fluid damper can dissipate a large amount of kinetic energy of the shell, and the cartridge lock can limit the rebound movement. The combination of the two ensures the smooth process of closing the breechblock. The research provides a design method for the process of the test shell entering the bore, and provides theoretical support for the feasibility of the method.     

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.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.     

美军建模与仿真管理特点及启示

美军是世界上唯一建立战争全域模拟仿真体系的军队,其建模与仿真建设高效管理的一些经验值得我军借鉴。本文归纳了美军建模与仿真管理5个方面的特点：高层机构统一领导,专职部门实施管理,以促进协作和共享为重点,规范化管理,模型、数据与服务一体化管理。并针对我军建模与仿真应用领域不广、协作共享不够、数据与服务管理欠缺的问题,提出了相应的建议。     

惯性导航系统故障诊断的不确定性问题研究

针对构造惯性导航系统 ( INS)故障诊断所面临的确定性和不确定性问题 ,提出了基于模糊集理论的诊断方法 ,并给出诊断系统自动获取不确定性证据和确定性证据隶属度的方法及函数 .认为对于确定性证据和不确定性证据可以用统一的方法和原则来处理 ,并建立了两类证据的实用数学模型     

大学计算机基础课程教材的建设与实践

面向21世纪计算机课程体系的核心是计算机层次教育.以1996～1998年出版的全军统编计算机教材和国家级"九五"重点计算机教材为基础,论述了计算机层次教育所包括的内容及具体的实施办法.     

直接网络中的自适应路由算法分析

互连网络是大规模并行计算机的重要组成部分，路由算法是其中决定网络性能的重要因素，本文在直接网络结构基础上对路由算法进行讨论，给出了一种分类方法，并着重对采用虫孔路由开关技术的自适应路由算法进行分析，为进一步的评价和设计新的算法提供了参考。     

分形信号的滤波算法

提出了分形信号的小波分解与重构的一种快速算法。针对分形信号的自相似和长时相关的特点，采用离散小波变换（DWT）对分形信号进行多尺度分解，使其成为各尺度上的近似平稳信号，从而可利用通常的Wiener滤波或Kalman滤波方法进行估计，然后再由DWT进行多尺度重构，估计出被噪声污染了的原始信号。重点对DWT的滤波过程进行算法设计，并估计了计算复杂度。     

双基地两坐标雷达空间目标定位算法

本文提出了双基地雷达单独使用发射／接收站（Ｔ／Ｒ站）的目标斜距和方位角信息或接收站（Ｒ站）的目标距离和方位角信息分别对空中目标的二维定位算法，并给出了定位精度的分析方法。最后，通过计算机仿真讨论了算法的定位性能。     

测量船中心机实时监控专家系统建造技术

测量船中心机实时监控专家系统应用于测量船中心机系统执行海上测量任务的时节，旨在提高整个系统的实时性和可靠性。本文围绕实时专家系统的时序性、时变性、时效性等特征，从系统设计与实现两个方面讨论建造该专家系统的一些关键技术。