复合材料超临界机翼跨音速颤振实验与数值计算研究

颤振课题是飞机设计过程中常常遇到的一个关键技术问题。以支线客机ARJ21超临界机翼颤振特性研究为背景,在俄罗斯TsAGI的T-106风洞中完成了该复合材料机翼跨音速颤振实验,基于N-S方程和无限插值方法（TFI）生成三维贴体运动网格对超临界机翼跨音速颤振进行了并行计算。结果表明：复合材料的超临界机翼在跨音速区域具有跨音速颤振＂凹坑＂现象;与风洞实验结果相比,有较好的一致性,为使用超临界机翼的运输类飞机跨音速颤振特性预计提供了一定的参考。     

Expanding global access to civilian and commercial remote sensing data: implications and policy issues

Current and planned developments in the field of civilian and commercial satellite imagery promise a major expansion in international accessibility to remote sensing data and technologies. This paper addresses the implications of the expanding global access to land remote sensing data and their derived products. While atmospheric, meteorological, and oceanographic data is also widely available at cost or free of charge, it is land remote sensing - specifically the unique systems with high-resolution and frequent revisit times - that are of primary concern for international and regional security issues. Military and intelligence satellites are not addressed in this discussion of expansion due to their inherently controlled access, unless such systems also provide commercially available imagery or products (as is the case with some Russian systems).     

The Induced Magnetospheres of Mars, Venus, and Titan

This article summarizes and aims at comparing the main features of the induced magnetospheres of Mars, Venus and Titan. All three objects form a well-defined induced magnetosphere (IM) and magnetotail as a consequence of the interaction of an external wind of plasma with the ionosphere and the exosphere of these objects. In all three, photoionization seems to be the most important ionization process. In all three, the IM displays a clear outer boundary characterized by an enhancement of magnetic field draping and massloading, along with a change in the plasma composition, a decrease in the plasma temperature, a deflection of the external flow, and, at least for Mars and Titan, an increase of the total density. Also, their magnetotail geometries follow the orientation of the upstream magnetic field and flow velocity under quasi-steady conditions. Exceptions to this are fossil fields observed at Titan and the near Mars regions where crustal fields dominate the magnetic topology. Magnetotails also concentrate the escaping plasma flux from these three objects and similar acceleration mechanisms are thought to be at work. In the case of Mars and Titan, global reconfiguration of the magnetic field topology (reconnection with the crustal sources and exits into Saturn??s magnetosheath, respectively) may lead to important losses of plasma. Finally, an ionospheric boundary related to local photoelectron signals may be, in the absence of other sources of pressure (crustal fields) a signature of the ultimate boundary to the external flow.     

复合材料胶接缺陷的红外热像检测

简要介绍了红外热像的检测原理，并用红外热像方法对铝蜂窝铝蒙皮复合材料较易出现的胶接缺陷进行检测，结果表明红外热像方法是检测复合材料胶接缺陷的快速、有效方法。不同性质缺陷的最佳检测时间不同，对于铝蜂窝铝蒙皮结构复合材料蒙皮的各种脱粘缺陷，检测速度都高于每分钟两屏。实现被检工件快速、方便、自动化的加热方式，加热源和热像头的同步自动扫查以及智能化地识别各种缺陷是今后红外热像检测发展的重要方向。     

应用CFD方法的舰载直升机舰面气弹响应计算与分析

舰载直升机所处的环境恶劣,易出现旋翼桨尖过度挥舞及机身碰撞等事故,研究直升机舰面气弹响应可预防此类事故的出现。应用 CFD 方法获得舰船流场数据,结合桨叶动力学模型,综合提出旋翼气弹响应计算分析方法,研究不同来流速度、悬停位置与风向角下旋翼的气弹响应。结果表明：本文提出的气弹响应计算分析方法正确可行;舰船来流速度的增加...     

某型飞机反推力装置加载试验

由于反推力系统必须在模拟气动载荷下做试验,以验证反推力系统功能的安全可靠性。因此在液压系统地面模拟试验中需配置一套反推力装置加载系统,以实现对反推力在展开和收起过程中所受气动载荷的模拟。在简要介绍反推力系统及其加载系统的基础上,主要研究如何完成某型飞机反推力装置加载试验,并满足其性能要求。     

高性能铝基复合材料的颗粒分布及界面结合

采用常规粉末冶金和高能球磨粉末冶金法制备了B4Cp/Al复合材料，研究了B4C颗粒分布与界面结合特点、形成机制以及对材料性能的影响。结果表明，17％（体积分数）B4Cp/6061Al复合材料的屈服和抗拉强度分别为415MPa和470MPa，比常规粉末冶金复合材料分别提高了69％和70％。微观分析表明，高能球磨粉末冶金复合材料中B4C颗粒均匀分布、颗粒与基体之间存在近百纳米厚度的界面层，界面层由呈带状且有序分布的微细铝晶粒和弥散分布的纳米颗粒组成。高能球磨过程中，铝粉末在钢球表面形成冷焊层，B4C不断被挤入而均匀化是实现颗粒均匀分布的主要机制；球磨过程中铝粉末表面氧化层破碎暴露出新鲜铝表面且与镶嵌与铝粉末中的B4C颗粒形成界面结合是获得良好界面结合复合材料的重要条件     

CCD互相关粒子图像测速及其在对抗流流场测量中的应用

在常规自相关粒子图像测速（ＰＩＶ）系统的基础上,发展了一个采用ＣＣＤ像机的互相关粒子图像测速系统。用这一新系统测量了对抗流流场的结果表明,这一技术克服了自相关粒子图像测速技术在测量具有滞止点的流场中的困难。实验说明,与自相关粒子图像测速技术相比,这一技术更快捷有效。     

High-frequency AC power distribution in Space Station

A utility-type, 20-kHz, AC power distribution system for the space station employing resonant power-conversion techniques is presented. The system converts raw DC voltage from photovoltaic cells or three-phase, low-frequency AC voltage from a solar dynamic generator into a regulated, 20-G kHz AC voltage for distribution among various loads. Operations of the components of the system such as driver inverter, DC receiver, bidirectional receiver, and three-phase AC receiver are discussed. EASY5 computer modeling and simulations were performed to study the local and global performance of the system. Simulation results show that the system has fast response and good transient behavior. The AC bus voltage is effectively regulated using the phase-control scheme, which is demonstrated with both line and load variations. The feasibility of paralleling the outputs of driver modules is illustrated with the driver modules synchronized and sharing a common feedback loop. A high-frequency, sinusoidal AC voltage is generated in the three-phase, AC input case, when the driver modules are phased 120° away from one another and their outputs are connected in series     

一种星载伞天线展开机构研究

天线展开机构使用动力绳实现天线展开和收拢过程中易出现动力绳松弛、脱槽现象。以星载高精度伞状天线展开机构为研究对象,分析天线展开机构的工作原理;利用解析法获得展开机构的运动方程,结合天线展开机构运动部件结构参数,得到天线展开过程中展开机构动力绳的松弛规律;建立以展开机构结构参数为设计变量,以动力绳松弛量最小为目标的展开机构结构优化模型,通过模拟退火法进行求解,得到优化的展开机构结构参数,通过优化前后的展开机构展开、收扰功能试验,测试了机构工作时动力绳的松弛量,验证了展开机构优化的正确性。结果表明：优化后的展开机构动力绳松弛量较优化前降低了90%,优化效果显著。