轴流压气机试验若干异常气动现象表征与机理分析

在梳理某压气机试验器开展的历次压气机性能试验结果基础上,分析了试验系统发生的若干典型异常气动物理现象,通过试验数据表征分析与抑制方法试验验证,初步揭示了压气机试验异常气动现象的形成机制.研究结果表明:进口局部导叶角度失调会对下游流场产生扰动,导致压气机性能与稳定性出现恶化;转子顶部容腔通道逆流是导致压气机转子前外壁静压测量值偏高的原因,通过抑制容腔逆流可以改善压气机气动性能;改变进口节流比观察换算流量是否发生变化,是判定压气机试验进气系统漏气问题的有效方法.研究结果对于指导压气机性能试验故障诊断和提高试验分析能力具有重要作用.      

基于ICCD的空间微光成像系统成像性能研究

研究基于像增强型CCD（ICCD）的空间高分辨率微光成像系统的成像性能。通过理论推导及数学仿真的方法，对系统在微光条件下的能量传递、极限分辨力、信噪比以及调制传递函数进行分析计算。研究表明，系统在黎明照度条件下具有较好探测能力，通过对ICCD器件制冷可以有效提高系统信噪比，实现满月照度的探测成像。     

高填充复合推进剂的初始粘弹性泊松比

本文从粘弹性力学和复合材料力学理论说明，高填充复合固体推进剂的初始粘弹性泊松比可能小于０．４，并讨论了粘弹性泊松比的测试方法，利用一种新方法得出了相应的实验数据。     

伴飞诱饵支援条件下无人飞行器协同作战效能研究

针对复杂的威胁环境，介绍了伴飞诱饵在体系作战条件下的应用情况；基于排队论的突防概率模型，研究了伴飞诱饵支援条件下，无人飞行器的协同突防概率和效费比：提出了作战体系作战时效性的概念；建立了火力对抗条件下无人飞行器打击防空导弹防御体系的Lanchester方程，利用所建模型分析了伴飞诱饵对作战时效性的贡献。研究表明，排队论和Lanchester方程用于伴飞诱饵条件下的无人飞行器协同作战效能研究是有效的。     

寻的导弹寄生天线罩耦合回路有效导航比设计

基于比例导引(PN)制导律和实际惯性稳定框架式导引头回路,针对导引头回路两种校正网络,建立了用于设计有效导航比的两种寻的导弹寄生天线罩耦合回路模型,给出了PN寻的制导系统的控制弹道实际有效导航比的计算公式及设计准则。算例结果表明,该方法正确有效,所得脱靶量较小。     

Azimuth selection for sea level measurements using geodetic GPS receivers

Based on analysis of Global Positioning System (GPS) multipath signals recorded by a geodetic GPS receiver, GPS Reflectometry (GPS-R) has demonstrated unique advantages in relation to sea level monitoring. Founded on multipath reflectometry theory, sea level changes can be measured by GPS-R through spectral analysis of recorded signal-to-noise ratio data. However, prior to estimating multipath parameters, it is necessary to define azimuth and elevation angle mask to ensure the reflecting zones are on water. Here, a method is presented to address azimuth selection, a topic currently under active development in the field of GPS-R. Data from three test sites: the Kachemak Bay GPS site PBAY in Alaska (USA), Friday Harbor GPS site SC02 in the San Juan Islands (USA), and Brest Harbor GPS site BRST in Brest (France) are analyzed. These sites are located in different multipath environments, from a rural coastal area to a busy harbor, and they experience different tidal ranges. Estimates by the GPS tide gauges at azimuths selected by the presented method are compared with measurements from physical tide gauges and acceptable correspondence found for all three sites.     

A novel environmental control system based on membrane dehumidification

This paper conducts a simulation study of a novel aircraft environmental control system based on membrane dehumidification(MD-ECS),and compares the system with the up-to-date four-wheel high pressure de-water system(4WHPDW-ECS).Mathematical models for the two systems are established,and a system simulation using a numerical technique is performed to analyze and compare the cooling performance of the two systems.Simulation results show that the cooling capacity of MD-ECS is much higher than that of 4WHPDW-ECS under the same working conditions,indicating that the novel system is theoretically feasible and promising.The effects of the sweep ratio of the membrane dehumidifier on the dehumidification and cooling performance of the system is also investigated.     

钛合金蜂窝三层结构的扩散焊接研究

介绍了俄罗斯钛合金蜂窝三层结构扩散焊接的研究成果.详细介绍了铝合金、焊接规范选择、接头应力变形状态的分析、模拟计算等,有助于国内钛合金的焊接研究.     

远程星际航行补篇

通过一系列变量置换推导出不同喷气速度和不同加速度条件下,计算恒星际飞船加速段的时间和距离的普遍公式及多级火箭加速情况下加速段的时间和距离的公式。最后以天狼星作为航行目标、计算了用5级和10级火箭加速飞行的时间和距离。结果表明,当火箭的级数很多,且各级加速度相等时,其飞行时间与距离非常接近匀加速飞行的情况。     

Lunar geophysical parameters inversion based on gravity/topography admittance and particle swarm optimization

This paper presents a FORTRAN computer program. The program as code will be used for lunar parameter inversions based on gravity/topography admittance. This will be done by assuming that the lunar lithosphere is modeled as a thin elastic spherical shell. The parameters discussed here include; load ratio, crustal thickness, subsurface load depth, crustal density and elastic lithosphere thickness. The admittance of the best-fitting model can be found through automatically adjusting misfits between one theoretical admittance and an observed one. The results in this paper indicate that this research’s theoretical model is reasonable for exploring the best-fitting parameters. In addition, this code is not only able to automatically and simultaneously calculate the global optimum solution of the parameters studied, but also performs well in computational speed. The code can be easily modified to include more parameter inversions; such as the inversion for subsurface density anomaly and the case of considering infilling material in some lunar mare basins.