陆军诸兵种合同作战兰切斯特方程的弹药消耗预测研究

描述了诸兵种合同作战的兰切斯特方程及其矩阵解,提出了一种通过兵力损耗换算弹药损耗的新思路,分析和确定了用该方法预测弹药消耗的相关参数,最后运用Matlab进行仿真计算,预测出了武器装备战损情况和弹药消耗情况。     

基于BP神经网络带调压器直流发电机特性的辨识

为使坦克直流发电机的调压特性实验能够在计算机上仿真进行,节约教学实验成本,可利用神经网络对直流发电机的调压特性进行辨识,得到了比手工绘制精度更高的特性曲线.因此,调压特性的神经网络辨识法,有利于直流发电机特性实验教学.     

SPC技术在导弹厚膜混合电路生产中的应用

SPC(统计过程控制)作为一种先进的质量管理方法,在国外企业被广泛采用,目前国内也有众多企业开始推行.分析了实施SPC的重要性,根据SPC技术在推广应用中的主要工作内容,给出了导弹厚膜混合电路生产中SPC技术的应用方法,包括关键工序节点和工艺参数的确定、工艺参数数据的采集、控制图的使用、工序能力评价以及所采用的控制技术等实际应用方面的内容.     

超空泡航行体双层壳结构动力稳定性分析

针对超空泡航行体轴向受力特点,建立超空泡航行体双层壳结构有限元模型,对结构动力稳定性进行分析.数值计算表明,当壳间实肋板厚度增大或环向肋骨数量和尺寸增加时,动力失稳区域整体下移,不稳定激发频率下降,失稳区域宽度减小幅度较小;当壳间间距减小或纵向肋骨数量和尺寸增加时,双层壳结构动力不稳定激发频率上升,动力失稳区域宽度较大...     

临近空间对地观测平台的矢量化建模及稳定性分析

研究了临近空间对地观测平台的矢量化建模和稳定性问题.定义了描述观测平台空间运动的坐标系及运动参数;在受力分析的基础上,根据Newton-Euler方程建立了矢量形式的六自由度非线性数学模型;基于此模型,应用Lyapunov稳定性理论对观测平台的稳定性进行了分析.研究结果表明:对于给定的未扰运动,观测平台是渐近稳定的;纵...     

美军作战实验室建设研究

简要回顾了美军作战实验发展的历史,从军种到联合详细阐述了美军作战实验室完整的体系,并简要介绍了各作战实验室所完成的典型实验,研究了美军作战实验室主要的实验方法和技术手段,剖析了美军作战实验室的运行机制,探讨了美军作战实验室建设带给我们的启示。     

探空火箭级间段的CAD系统

本文在CADKEY绘图软件包的支持下,开发了加筋圆柱结构CAD系统—Hcadx.此系统通过菜单引导用户的操作,可用经验公式或解析法作轴压稳定分析,用罚函数法优化参数,可以在不退出Hcadx的情况下启动CADKEY,自动绘制设计草图。此草图经过适当地编辑、修改、便可成为工程中能接受的工作图纸。     

无奇点三维攻击时间控制滑模导引律

为研究导弹在视场角约束下的三维攻击时间控制问题,提出一种三维非线性滑模导引律。利用攻击时间误差设计滑模面,推导出三维形式的俯仰和偏航加速度指令;通过对所设计制导律进行简单修正,解决了零初始前置角引起的奇点问题;从数学上证明了该导引律的稳定性和收敛性,讨论了导引律相关参数的取值范围,分析了与纯比例导引法、解耦三维导引律之间的关系。仿真结果表明,所设计导引律能够在视场角约束条件下有效实现攻击时间增大或减小的控制;俯仰和偏航平面的耦合程度越强,该导引律控制能耗小的优势越为明显。     

Multi-objective design optimization of composite submerged cylindrical pressure hull for minimum buoyancy and maximum buckling load capacity

This paper presents the design optimization of composite submersible cylindrical pressure hull subjected to 3 MPa hydrostatic pressure. The design optimization study is conducted for cross-ply layups [0s/90t/0u], [0s/90t/0u]s, [0s/90t]s and [90s/0t]s considering three uni-directional composites, i.e. Carbon/Epoxy, Glass/Epoxy, and Boron/Epoxy. The optimization study is performed by coupling a Multi-Objective Genetic Algorithm (MOGA) and Analytical Analysis. Minimizing the buoyancy factor and maximizing the buckling load factor are considered as the objectives of the optimization study. The objectives of the optimization are achieved under constraints on the Tsai-Wu, Tsai-Hill and Maximum Stress composite failure criteria and on buckling load factor. To verify the optimization approach, optimization of one particular layup configuration is also conducted in ANSYS with the same objectives and constraints.     

Effect of organo-modified montmorillonite nanoclay on mechanical,thermal and ablation behavior of carbon fiber/phenolic resin composites

The mechanical, thermal and ablation properties of carbon phenolic (C-Ph) composites (Type-I) rein-forced with different weight percentages of organo-modified montmorillonite (o-MMT) nanoclay have been studied experimentally. Ball milling was used to disperse different weight (wt) percentages (0, 1,2,4,6 wt.％) of nanoclay into phenolic resin. Viscosity changes to resin due to nanoclay was studied. On the other hand, nanoclay added phenolic matrix composites (Type-II) were prepared to study the dispersion of nanoclay in phenolic matrix by small angle X-ray scattering and thermal stability changes to the matrix by thermogravimetric analyser (TGA). This data was used to understand the mechanical, thermal and ablation properties of Type-I composites. Inter laminar shear strength (ILSS), flexural strength and flexural modulus of Type I composites increased by about 29％, 12％and 7％respectively at 2 wt.％ addition of nanoclay beyond which these properties decreased. This was attributed to reduced fiber volume fraction (％Vf) of Type-I composites due to nanoclay addition at such high loadings. Mass ablation rate of Type-I composites was evaluated using oxy acetylene torch test at low heat flux (125 W/cm2) and high heat flux levels (500 W/cm2). Mass ablation rates have increased at both flux levels marginally up to 2 wt.％ addition of nanoclay beyond which it has increased significantly. This is in contrast to increased thermal stability observed for Type-I and Type-Ⅱ composites up to 2 wt.％addition of nanoclay. Increased ablation rates due to nanoclay addition was attributed to higher insulation effi-ciency of nanolcay, which accumulates more heat energy in limited area behind the ablation front and self-propagating ablation mechanisms triggered by thermal decomposition of organic part of nanoclay.