汽车超车过程的空气动力特性研究

采用稳态和瞬态两种方法,对两辆车超车过程中外部流场的空气动力特性进行了数值模拟研究。采用网格变形和局部网格重构相结合的动网格技术,并耦合刚体动力学方程和PISO算法实现了汽车超车过程的三维瞬态数值模拟。通过稳态和瞬态计算,探讨了超车过程中两车纵向相对位置对气动特性的影响以及气动力对汽车行驶稳定性的影响。研究发现超车过程中被超车的阻力、侧向力和横摆力矩都有最大值,并找出了其变化规律。通过对稳态与瞬态计算结果的比较,可以看出:本文采用的瞬态模拟方法能够充分捕捉超车过程中的动态效应,优于传统的稳态模拟。     

基于IP网络的测试研究

为实现IP语音测试的专项研究,介绍了基于VOIP(Voice over IP IP语言)的信令及语音测试相关技术实现方案,系统硬件及功能实现框图。对IP语音测试平台的硬件设计方法及语音质量测试(VQT),信令流及媒体流的测试模型进行了研究。     

基于交交变频的静止进相器研究

阐述了异步电动机无功补偿的原理,提出了通过交交变频实现异步电动机无功功率补偿的方法。系统采用单片机控制,能够实现自动跟踪、自动补偿以达到提高电动机功率因数、降低电机定子电流、电机温升等目的。     

Influence of aircraft surface distribution on electromagnetic scattering characteristics

In this paper, two typical stealth aircraft concepts (wing fuselage blended and flying-wing) were designed. Then three gradually changed surface distribution models with the same plan-form for each concept were created. Based on the multilevel fast multipole algorithm (MLFMA), the vertical polarization transmitting/vertical polarization receiving (VV) and horizontal polariza-tion transmitting/horizontal polarization receiving (HH) radar cross section (RCS) characteristics were simulated with five frequencies between 0.1 and 1.0 GHz. The influences and mechanisms of aircraft surface distribution on electromagnetic scattering characteristics were investigated. The results show that for the wing fuselage blended concept, the VV RCS of this frequency range is higher than the HH RCS in most cases, while it is just the opposite for the flying-wing concept. As for the two aircraft concepts, the RCS levels of HH and VV both decrease with the frequency increasing, but the HH RCS has a faster downward trend. The surface distribution has little influ-ence on HH RCS characteristics. On the contrary, it has a significant impact on VV RCS charac-teristics, and the amplitude of the VV RCS increases with the surface thickness.     

A passive tracking filter for missile capture

A practical filter is suggested for ground-based missile tracking in a capture-guidance mode utilizing angle-only measurements from a passive missile sensor, and its performance is evaluated by a realistic system-simulation study. A missile-acceleration model that provides inputs to the filter is also suggested. The filter has a decoupled structure of independent azimuth and elevation channels, which requires fewer computations in solving the filter gain compared to a coupled structure. Simulation results show good tracking performance of the filter when used in association with the proposed missile-acceleration model     

三层客户／服务器模式分布式应用中的技术难点

本文介绍了在三层客户机／服务器模式分布应用开发中遇到的几个问题及解决办法。     

从美国两个传感器会议看新型传感器发展趋势

本文介绍了1990年9月在美国芝加哥举行的国际传感器展览会与克里夫兰举行的第三届国际化学敏传感器学术交流会议的概况。从会议展出的产品中概括、总结了美国传感器目前达到的水平与几类新型传感器的发展情况(如微结构传感器、光纤传感器、有机薄膜传感器、硅传感器与化学敏传感器),可供国内同行借鉴。     

实验应力分析处理中电子表格应用简介

简述了实验应力分析中电子表格的建立和应用，该表格方式可使数据处理，应力分析简捷明了计算结果形象直观。     

Performance analysis of PNG laws for randomly maneuvering targets

The performance of the conventional proportional navigation guidance (PNG) law for a randomly maneuvering target is considered. By means of the Lyapunov method, it is proved that an ideal missile guided by the conventional PNG law can always intercept a target which maneuvers with time-varying normal acceleration provided that the navigation constant is sufficiently large. The authors also propose a modified PNG (MPNG) law which seems to improve the performance of the conventional PNG law at the final phase of pursuit. Simulation results demonstrate that the MPNG law demands less missile acceleration at the final phase of pursuit than the conventional PNG law     

Au基六元合金中的Ni固溶体研究

本文运用TEM.EDS等微观分析手段对Au基六元合金中的Ni固溶体进行了研究。结果表明,Ni固溶体为f,c,c结构(a_(Ni)=0.355nm).经调幅分解形成的置换式固溶体,成分为65at％Ni,10at％Au,18at％Fe,7at％cr,与基体有如下取向关系:(11-1)_(Ni)∥(11-1)_(Au),[011]_(Ni)∥[011]_(Au)。Ni固溶体在合金中起界面强化和弥散强化作用。