High speed driving of a gain-switched laser diode with anexponential transmission line

With the increase of information capacity of an airborne system, high speed driving of laser diodes have been of interest. In order to match the low resistive LD, proposed in this paper is an exponential transmission line, which is used as preshaping to compensate the pattern effect in gain switching of laser diodes. It also will be used to overcome the effect of parasitic elements in high speed driving to improve the rise and trail edges of the output waveform. An accurate circuit model of the exponential line for the PSPICE program has been developed and simulations are conveniently carried out by employing PSPICE     

Estimation of ground range on the sweep frequency backscatter leading edge

The high frequency management system with backscatter radar supplies the real time ionosphere channel conditions to high frequency users, which leads to the demand for the ground range between the radar location and the scatters on the distant ground. The ionosphere electron density profile is usually inversed to obtain the ground range. An inversion algorithm, with which the ground range on the leading edge of the backscatter ionograms can be obtained without electron density, is presented in this paper. The ray path geometry of the backscatter sounding and the change in the group path on the leading edge with operating frequency are used to derive the ground range. Synthesized backscatter ionogram and experimental backscatter ionograms are processed to validate the algorithm. The results indicate that the algorithm is usable for high frequency management system.     

压气机叶栅中应用弯曲叶片的研究

从弯曲叶片控制叶栅二次流的机理出发,讨论了压气机叶栅中应用弯曲叶片的特殊性,并根据国内外的有关文献和通过实验所取得的研究结果,分析了压气机叶栅中应用弯曲叶片的国内外研究现状、实际应用情况及未来的发展前景。     

China's Future Missions for Deep Space Exploration and Exoplanet Space Survey by 2030

Four future missions for deep space exploration and future space-based exoplanet surveys on habitable planets by 2030 are scheduled to be launched. Two Mars exploration missions are designed to investigate geological structure, the material on Martian surface, and retrieve returned samples. The asteroids and main belt comet exploration is expected to explore two objects within 10 years. The small-body mission will aim to land on the asteroid and get samples return to Earth. The basic physical characteristics of the two objects will be obtained through the mission. The exploration of Jupiter system will characterize the environment of Jupiter and the four largest Moons and understand the atmosphere of Jupiter. In addition, we further introduce two space-based exoplanet survey by 2030, Miyin Program and Closeby Habitable Exoplanet Survey (CHES Mission). Miyin program aims to detect habitable exoplanets using interferometry, while CHES mission expects to discover habitable exoplanets orbiting FGK stars within 10 pc through astrometry. The above-mentioned missions are positively to achieve breakthroughs in the field of planetary science.     

页轮干式磨削Ti6Al4V合金

进行了Ti6A14V合金锆刚玉页轮和碳化硅页轮的磨削性能试验研究,分析了磨削用量对磨削力、磨削温度和磨削表面完整性的影响。磨削力通过KISTLER9265B测力仪测定,磨削表面温度由NIUSB-621X信号采集系统测得,磨削表面形貌和金相组织由HiroxKH-7700型体视显微仪和Quanta200型扫描电镜（SEM）观察,表面粗糙度由Mahr Perthometer M1粗糙度仪测得,表层显微硬度通过HVS—1000硬度计测定。研究结果表明：页轮磨削钛合金工件表面没有发生烧伤现象,磨削热影响区厚度小于50μm,锆刚玉页轮比碳化硅页轮更适合干式磨削钛合金。     

一种求解核函数方程的新方法—辅助核法

本文提出了求解核函数方程的辅助核法。此法克服了偶极子栅格法对网格分布的限制,具有更大的适用范围。数值计算表明,此法对求解绕翼型的跨声速激波流动是很有利的。     

运输飞行成本指数计算

对运输飞行成本进行了划分,提出了计算成本指数的方法,分析了成本指数对运输飞行经济性的影响。以某航空公司为例,计算了该航空公司的成本指数,并在全飞行模拟机上验证了使所计算的成本指数飞行的运输飞行成本。结果表明,使正确的成本指数飞行,将大量节约运输飞行成本。可为航空公司计算自己的成本指数,降低成本,提高运输飞行经济性提供参考。     

双功能陶瓷膜生物反应器处理污水的实验研究

针对目前膜生物反应器运行过程中膜易污染的问题，研制了一种新型的双功能陶瓷膜生物反应器．该生物反应器的主要特点是采用一种具有双重功能的陶瓷膜作为生物反应器的主要元件，陶瓷膜可以交替地进行曝气和过滤，将膜的在线反冲清洗和生物反应器的供氧曝气结合在一起．考察了不同运行条件下该反应器对COD、氨氮的去除效果．对陶瓷膜的充氧能力进行了实验，测得小孔陶瓷膜、大孔陶瓷膜、砂型曝气头的氧传递系数分别为：0．2315min-1，0．1587min-1，0．0991min-1．     

基于超精密应用的高刚度高阻尼空气静压导轨研究

介绍了一种采用多孔质节流的新型空气静压导轨,其刚度可以达到400N/μm或者更高,具有这种刚度的空气静压导轨可以取代液体静压导轨,广泛应用于超精密机床中.     

考虑配平特性的超声速客机低声爆气动布局优化研究

降低声爆水平是下一代超声速运输机研制需要解决的关键问题之一。低声爆优化通常使飞行器布局向着机翼后掠角增大、机翼沿机身方向分布范围增大的趋势发展,给飞行器的配平和低速特性带来不利影响。以某超声速客机基本构型为研究对象,建立基于类别/形状函数的翼身组合体参数化建模方法;基于超声速线化理论分析外形几何参数对声爆水平的影响。在此基础上,分别针对机身轮廓、机翼平面形状以及扭转角分布对该构型进行低声爆优化和俯仰力矩特性优化,并采用CFD 方法对优化结果进行校核。结果表明：与基准构型相比,在不显著增加俯仰力矩的基础上,优化构型的阻力降低了19 cts,近场过压显著降低,地面声爆响度降低5.1 PLdB。