真空羽流污染的数值模拟

姿控发动机真空环境下工作产生的喷流对航天器造成的污染非常严重.根据污染的性质,羽流污染又分为机械污染、热污染、沉积污染和化学污染.用直接模拟的蒙特卡罗(DSMC)法数值求解真空羽流场,在此基础上计算热污染和沉积污染,将对空间飞行器的设计和科学实验有参考价值.      

PZT/PVDF压电复合材料的合金化制备技术及其性能研究

采用氧化物球磨法制备了ＰＺＴ粉末,ＸＲＤ显示它是Ｚｒ与Ｔｉ比例为５２：４８的纯四方钙钛矿型结晶相,用合金化技术获得了六种含ＰＺＴ不同体积分数的ＰＺＴ／ＰＶＤＦ复合材料,对其介电性和压电性的测试表明,随着ＰＺＴ含量的增加,电性能参数呈非线性增大,当ＰＺＴ的体积分数达到７０％时,介电常数ε和压电常数ｄ３３值迅速增加并接近纯ＰＺＴ值。     

SHS/PHIP合成TiC-Al2O3-xFe金属陶瓷的工艺及性能

采用ＳＨＳ／ＰＨＩＰ工艺制轩出了致密的ＴｉＣ－Ａｌ２Ｏ３－ｘＦｅ金属陶瓷。研究子延迟时间、高压持续时间及压力等工艺参数对合成ＴｉＣ－Ａｌ２Ｏ３－２０Ｆｅ金属陶瓷密度的影响,并分析了Ｆｅ含量对ＴｉＣ－Ａｌ２Ｏ３－ｘＦｅ金属陶瓷材料性能的影响。     

燃烧合成TiN陶瓷

采用燃烧合成工艺制备ＴｉＮ陶瓷件。压坯由７０μｍＴｉ加１５μｍＴｉＮ稀释剂经干压而成,孔隙率为４５％。压坯与８０ＭＰａＮ２反应合成ＴｉＮ陶瓷件。密度为理论密度的７５％。稀释剂为１５μｍ ＴｉＮ粉末,是由７０μｍＴｉ粉与８ＭＰａＮ２反应合成。对产物进行了ＸＲＤ相分析和ＳＥＭ微观组织分析。     

The relationship between ionospheric total electron content (TEC) over East Asia and the tropospheric circulation around the Qinghai-Tibet Plateau obtained with a partial correlation method

This paper reports a study on the relationship between ionospheric total electron content (TEC) over East Asia and the tropospheric circulation around the Qinghai-Tibet Plateau. Ionospheric TEC over East Asia are obtained from 25 observatories during 1996–2004. By applying a partial correlation method which can eliminate the influences of solar and geomagnetic activities, we find no significant correlation between TEC and the Asian zonal circulation index (Iz), but find a positive correlation between the day-to-day variability of TEC and Iz. We suggest that the positive correlation is closely related with the topography of the Qinghai-Tibet Plateau. The dynamical effect on airflow of the plateau can generate vortexes, and the vortexes may continuously excite internal gravity waves (IGWs) which transmit up to the ionosphere and cause regional wave disturbances. This study gives evidence for the dynamical mechanism of ionosphere–troposphere coupling and shows the importance of the Qinghai-Tibet Plateau in the ionosphere–troposphere coupling over East Asia.     

利用多个相参脉冲回波估计目标径向速度和加速度

为从高加速度目标的多个相参脉冲回波中估计目标径向速度和加速度,首先对高加速度目标回波特点进行分析,其次提出采用FRFT(Fractional Fourier Transform)变换方法来提取目标径向速度、加速度,仿真结果验证了算法的有效性。     

一种新的仿真组件模型及其实现

为了提高仿真组件的重用性、兼容性,给仿真应用提供通用的开发模型,使仿真系统独立于仿真中间件,提出了一个新的自包含仿真组件模型,该模型由服务端口、适配器和调度引擎构成。而模型的描述采用静态结构和动态行为元元模型。开发时首先采用面向组件的建模工具描述系统的静态结构和动态行为,根据静态结构自动生成应用代码和适配器。其中适配器是联系仿真组件和仿真中间件的纽带,使它们彼此独立。运行时调度引擎将仿真组件装配到应用框架中并根据动态行为模型调度组件运行。实践表明该模型是一个适用于不同仿真中间件的标准模型,可以提高仿真模型的协同能力和重用性。     

轴流状态下涵道螺旋桨增升方法的数值模拟

为了进一步提高涵道螺旋桨的功率载荷,提出了一种将螺旋桨部分桨尖嵌入到涵道体内壁面以改善涵道内部的滑流边界和唇口扰流的增升方法。采用计算流体力学(Computational fluid dynamic, CFD)方法,对其轴流状态的流场流态及气动力特性进行了计算和分析,并与相同直径的孤立螺旋桨及涵道螺旋桨在相同工况下的气动力进行了对比分析。     

A Hitch-hiker’s Guide to Stochastic Differential Equations

In this review, an overview of the recent history of stochastic differential equations (SDEs) in application to particle transport problems in space physics and astrophysics is given. The aim is to present a helpful working guide to the literature and at the same time introduce key principles of the SDE approach via “toy models”. Using these examples, we hope to provide an easy way for newcomers to the field to use such methods in their own research. Aspects covered are the solar modulation of cosmic rays, diffusive shock acceleration, galactic cosmic ray propagation and solar energetic particle transport. We believe that the SDE method, due to its simplicity and computational efficiency on modern computer architectures, will be of significant relevance in energetic particle studies in the years to come.     

基于自动丝束铺放技术的复合材料进气道结构设计及试验验证

某型号飞机采用S形进气道,形状复杂,且对刚度、装配、内表面质量及重量要求很高,需要设计一个满足所需的进气道结构.采用复合材料整体成型结构设计,结合自动丝束铺放技术,详细叙述进气道结构设计研制方案及实施方法,并对其进行有限元理论分析及试验验证,结果表明:进气道结构满足强度及刚度要求;自动丝束铺放技术可以有效应用于变截面S形进气道研制.研究结果可对研制其他复杂形状飞机进气道提供依据.