随动定向战斗部破片飞散特性研究

针对防空导弹常规破片式杀伤战斗部使用中存在能量利用率低的缺陷,提出采用随动定向战斗部的观点。建立随动定向战斗部的破片动态飞散区和飞散速度的计算模型,采用数值解析方法,解决在复杂弹目交会条件下破片的飞散区域与打击速度的计算问题．并用MATLAB软件对建立的模型进行验证,得出仿真结果与实际结果一致,这表明模型是合理、正确的。     

视频载体的视觉暗示方法

暗示是用间接、含蓄的方法对受众进行说服和引导的一种传播手段.对目前视频载体的视觉暗示方法进行了总结,并以此提出了3个层级的暗示方法概念体系:情景级暗示、元素级暗示和显示级暗示,分别从语义表达和物理呈现两个方面来实现暗示.然后,对基于视频的视觉心理暗示在心理战中的应用进行了分析和展望.     

基于小波变换和中值滤波的无人机图像去噪算法

在无人机航拍图像的实时传输过程中,有可能会同时受到脉冲和高斯混合噪声的污染,为后续图像的识别造成很大的困难.针对这种情况,提出了一种基于中值滤波和小波变换相结合的图像去噪方法.仿真结果表明,该方法不仅能有效地滤除脉冲和高斯的混合噪声,而且可以很好地保留图像的细节信息,改善图像的视觉效果.     

Theoretical and numerical simulation study on jet formation and penetration of different liner structures driven by electromagnetic pressure

The use of a shaped liner driven by electromagnetic force is a new means of forming jets. To study the mechanism of jet formation driven by electromagnetic force, we considered the current skin effect and the characteristics of electromagnetic loading and established a coupling model of"Electric—Magnetic—Force"and the theoretical model of jet formation under electromagnetic force. The jet formation and penetration of conical and trumpet liners have been calculated. Then, a numerical simulation of liner collapse under electromagnetic force, jet generation, and the stretching motion were performed using an ANSYS multiphysics processor. The calculated jet velocity, jet shape, and depth of penetration were consistent with the experimental results, with a relative error of less than 10％. In addition, we calculated the jet formation of different curvature trumpet liners driven by the same loading condition and ob-tained the influence rule of the curvature of the liner on jet formation. Results show that the theoretical model and the ANSYS multiphysics numerical method can effectively calculate the jet formation of liners driven by electromagnetic force, and in a certain range, the greater the curvature of the liner is, the greater the jet velocity is.     

Prediction of three-dimensional elastic behavior of filament-wound composites based on the bridging model

This work provides a method to predict the three-dimensional equivalent elastic properties of the filament-wound composites based on the multi-scale homogenization principle.In the meso-scale,a representative volume element(RVE)is defined and the bridging model is adopted to establish a theoretical predictive model for its three-dimensional equivalent elastic constants.The results obtained through this method for the previous experimental model are compared with the ones gained respec-tively by experiments and classical laminate theory to verify the reliability of this model.In addition,the effects of some winding parameters,such as winding angle,on the equivalent elastic behavior of the filament-wound composites are analyzed.The rules gained can provide a theoretical reference for the optimum design of filament-wound composites.     

Investigate the effects of magnetic fields on the penetration ability of a shaped charge jet at different standoffs

The influence of a magnetic field on the stability of a shaped charge jet is experimentally investigated at standoffs of 490, 650 and 800 mm. The experimental results without and with the magnetic field are compared in terms of the shaped charge jet form, stability and penetration ability. A theoretical model based on one-dimension fluid dynamics is then developed to assess the depth of penetration of the shaped charge at those three standoffs and magnetic conditions. The results show that the penetration capability can be enhanced in more than 70% by the magnetic field. The theoretical calculations are compared with the experimental results with reasonably good correlation. In addition, the parameters introduced in the theory are discussed together with the experiments at three standoffs studied.     

N、P源对微生物法处理石油烃效果的影响

在微生物法处理石油烃的过程中,微生物对N、P源的供给非常敏感,不同的微生物对不同的N、P源的生物利用度是不相同的,N、P源的选择对降解效果有较大影响,所以有必要对最佳的N、P源进行筛选。对N、P源的逸择和加入量对降解效果的影响进行了研究,确定了最佳的N、P源分别为(NH4)2SO4、KH2PO4。在(NH4)2SO4、KH2PO4的质量浓度分别为100mg／L和60mg／L时,废水中石油烃的去除率最高。     

排队论在导弹防御体系射击效能中的应用

针对当前空袭手段多样化、综合化和一体化的特点,运用排队论方法,设计了一种基于排队论的射击效能评估模型。该模型综合考虑了各种因素对舰空导弹射击效能的影响,当编队的配置(如防御层数、通道数量)有所变化时,依然可以灵活运用上述模型对编队射击效能做出准确评估。     

三坐标雷达目标真实高度估计算法研究

在目标跟踪领域,通过三坐标雷达的测量值(斜距、仰角及方位角)来估算目标的真实高度一直是个难点。目前主要有两类处理方法:坐标转换法和等效地球半径法。前者把与雷达天线相关的三坐标测量值转换到大地坐标系统来计算目标高度;后者充分考虑地球曲率以及大气折射的特性,通过增加地球半径来估算目标的高度。最后对上述的两类方法进行总结、比较与分析。     

齿轮啮合温升模型建立及仿真研究

借助动力学仿真软件ADAMS,建立了齿轮啮合传动仿真模型。提出了一种计算高速齿轮传动轮齿瞬现温升的方法,基于齿轮啮合原理和M atlab计算软件平台,建立了轮齿瞬现温升计算模型。实现了完整齿面各啮合点切向速度、摩擦系数、接触带半宽和法向载荷等参数的计算。运用B lock接触温度准则,得出齿轮各啮合点瞬现温升及接触温度变化的仿真分析结果,为齿轮传动结构的合理优化设计提供科学依据。