动态多因子相关算法及其改进

以组网雷达情报综合处理为背景,针对多站多目标航迹相关问题,首先介绍了动态多因子相关算法的基本原理,然后在此基础上提出了几点改进措施。利用位置因子的重要性对相关判定区域做了限制;利用航向因子对判决结果进行二次修正,同时结合目标的机动检测问题,提高了对目标强机动的检测能力;此外,根据实验结果还对综合处理中的航迹配对准则进行了修正。通过算法的改进不仅改善了航迹相关的质量,还降低了运算量。最后给出了改进后的算法流程图。     

槽头式野战管线水击波速测量研究

液体管道的水击波速受流体压力、温度、分子结构、含气量及管线几何尺寸、管材等因素的影响,准确地确定管线的水击波速是一个相当困难的问题,通过实验测量水击波速是一个常用方法。管线水击波速的常用测量方法有波前法和周期法。综合运用波前法和周期法,设计了实验测量野战管线的水击波速,并将实验结果与笔者先前提出的水击波速计算公式的计算结果作了对比,验证了公式的有效性。     

稀土(R)-铁金属间化合物中的磁相互作用

利用两格点分子场论(MFT),比较了R_nFe_m(n/m=1/3,6/23)和R_nFe_mM_k(M:类金属或其他金属;n/m/k=2/14/1;1/10/2)(即RFe_3,R_6Fe_(23),RFe_(10)V_2,RFe_(10)Mo_2,RF_(10)V_2N_x)两类化合物分子间的磁耦合系数;给出了Fe—Fe、R—R和R—Fe相互作用对居里温度的不同贡献。     

基于自由边控制流图的路径覆盖分析实现方法

针对路径覆盖测试,给出了一般循环结构的一种简化处理方案及把按此方案得到的控制流图转化为自由边控制流图方法,并探讨了基于自由边控制流图进行路径覆盖分析的实现方法和优点。     

静态电磁场数值分析方法比较

从有限差分法、有限元法、边界元法和模拟电荷法这四种典型数值分析方法出发,简要介绍了静电场数值分析的原理。比较了各种算法与其适用范围的差异,并对其进展进行分析。最后,总结了目前静电电磁场数值分析方法研究中需要解决的问题。     

运动舰船的电场测量

从理论和实验上对起源于防腐措施的舰船电场已进行了一些研究,但主要是针对近场,实测也是在静态进行．对运动舰船的电场分布、数量级及信号形式尚未见到文献报道．作者根据一次对海上运动舰船的电场测量结果,对上述问题作了一些研究．依据实验现象和测量到的信号特征,提出初步理论分析．理论分析与实验数据基本符合,说明运动舰船产生的感应电场是可以测量的．     

磁悬挂天平偏航电磁场的二维有限元分析

在磁悬挂天平偏航控制中,偏航线圈中的电流变化对模型姿态变化影响十分显著.为了提高天平的偏航控制精度,有必要对天平偏航电磁场进行更为精确的分析.该文采用有限单元法对磁悬挂天平偏航电磁场进行了分析,得到了比传统计算方法更为准确的结果,并在实验中进行了验证,从而为磁悬挂天平的偏航控制提供了参考.     

Effect of tongue clearance on hydraulic performance of double support vortex pump

In order to study influence of tongue clearance on the hydraulic performance of double support vortex pump, three dimensional flow model with symmetric variable size tongue clearance was established by changing section parameter of tongue clearance, and applied to numerically simulate the steady inner flow in a vortex pump based on fixed working conditions and impeller through ANSYS FLUENT. The numerical results show the influence of tongue channel with two sections (non-uniform and uniform sections) on flow field characteristics in vortex pump. Firstly, the variation of tongue channel section changes the vortex structure distribution in circumferential flow channel. Specifically the spiral forward vortex structure in the circumferential direction shifts to large radius side with increasing tongue width. Secondly, the circumferential velocity gradient and axial pressure gradient both diminish with the increase of the tongue section, and the inlet/outlet pressure difference and velocity distribution also reduce with increasing tongue channel section. Finally, for vortex pump with non-uniform section of tongue channel, the head diminishes and the efficiency remains constant approximately with the increase of the tongue width, while the head and the efficiency both diminish for uniform section of tongue channel.     

Modeling of the whole process of shock wave overpressure of free-field air explosion

The waveform of the explosion shock wave under free-field air explosion is an extremely complex problem. It is generally considered that the waveform consists of overpressure peak, positive pressure zone and negative pressure zone. Most of current practice usually considers only the positive pressure. Many empirical relations are available to predict overpressure peak, the positive pressure action time and pressure decay law. However, there are few models that can predict the whole waveform. The whole process of explosion shock wave overpressure, which was expressed as the product of the three factor functions of peak, attenuation and oscillation, was proposed in the present work. According to the principle of explosion similarity, the scaled parameters were introduced and the empirical formula was absorbed to form a mathematical model of shock wave overpressure. Parametric numerical simulations of free-field air explosions were conducted. By experimental verification of the AUTODYN numerical method and comparing the analytical and simulated curves, the model is proved to be accurate to calculate the shock wave overpressure under free-field air explosion. In addition, through the model the shock wave overpressure at different time and distance can be displayed in three dimensions. The model makes the time needed for theoretical calculation much less than that for numerical simulation.     

多孔介质中气体流量对流动阻力影响的实验研究

对空气在多孔介质(Pd/SiO2颗粒催化剂)中的流动阻力特性进行了冷态实验,研究了气体流量对流动阻力的影响.结果表明:催化剂厚度一定时,随着气体流量增大,多孔介质中的流动阻力也逐渐增大.经过与经典阻力计算公式对比,分析了偏差影响因素.最后,结合实验数据拟合出了适合管式反应器中流动阻力计算的半经验公式,能精确地预测颗粒填...