用相位偏移干涉法精确测量量块长度

讨论了相位偏移干涉技术的原理、常用的算法和小数重合法的应用。在分析了传统的柯氏干涉仪的量块测量方法基础上 ,提出运用相位偏移干涉法的量块测量法 ,最后给出了量块测量的数据。     

利用压缩网格方法提高旋转声源定位计算效率

利用两种压缩网格方法:基于传统波束形成的CG2压缩网格方法和基于小样本数据的CG4压缩网格方法,对经典时域旋转声源波束形成(ROSI)算法进行优化加速。实验结果表明:两种压缩网格方法均不影响ROSI算法旋转声源定位效果,基于传统波束压缩形成的CG2网格方法能够提高ROSI算法的旋转声源定位计算效率1～2倍,基于小样本数据的CG4压缩网格方法能够提高ROSI算法的旋转声源定位计算效率13～18倍。除此之外,基于小样本数据的CG4压缩网格方法在相控麦克风阵列平面与旋转声源平面垂直条件下,仍能准确进行旋转声源定位。      

高重复频率DPL激光辐照光学薄膜元件温升规律实验研究

光学薄膜是激光系统中最易损坏的薄弱环节。在高重复频率脉冲激光辐照下光学薄膜表面温度急剧上升,导致膜层应力、结构发生变化,最后出现宏观的灾难性损伤。文章采用红外热像仪实时测量了重复频率10 kHz 的DPL脉冲激光辐照下光学薄膜元件表面激光辐照中心点的温度变化,分析了影响薄膜元件温度变化的众多因素。结果表明,采用热导率较大的材料作基板的薄膜样品表面的温升较低;基板厚度越大的薄膜样品表面温升越低;薄膜表面激光辐照中心点的温度与样品的吸收峰值功率密度呈线性关系。     

Temporal evolution of the RCS of aircraft wake vortices

Knowledge of the radar scattering characteristics is one of the key issues for the development of wake vortex detection technology. This paper studies the temporal evolution of the RCS (radar cross-section) of wake vortices. The RCS–time plot is observed to increase as a whole and step at a certain time. These properties could provide help to the design of wake vortex detection radar and the optimization of radar station layout. The special spiral structures within the wake, together with the Bragg scattering theory, are used to well explain these phenomena, and some representative radar experiments are also included to verify them.     

脉冲多普勒雷达特征提取技术分析

为了准确快速地对脉冲多普勒雷达进行识别,选择3个具有代表性的参数:相参性、脉内调制特性及脉冲重复频率进行提取,并讨论了各参数提取的几类理论研究和比较成功的应用方法,分析了脉冲多普勒雷达识别技术中存在的难点及发展方向.     

高效液相色谱仪色谱采集和控制卡

本文介绍了一种ＰＣ总线色谱采集和控制卡的设计和工作原理,带有此卡的ＰＣ机可实现与岛津高效液相色谱仪配套的专用色谱数据处理装置Ｃ－Ｒ３Ａ的功能,并可以和该色谱仪组成一完整系统,协同工作。     

Simulation of underexpanded supersonic jet flows with chemical reactions

To achieve a detailed understanding of underexpanded supersonic jet structures influenced by afterburning and other flow conditions, the underexpanded turbulent supersonic jet with and without combustions are investigated by computational fluid dynamics(CFD) method.A program based on a total variation diminishing(TVD) methodology capable of predicting complex shocks is created to solve the axisymmetric expanded Navier–Stokes equations containing transport equations of species. The finite-rate ratio model is employed to handle species sources in chemical reactions. CFD solutions indicate that the structure of underexpanded jet is typically influenced by the pressure ratio and afterburning. The shock reflection distance and maximum value of Mach number in the first shock cell increase with pressure ratio. Chemical reactions for the rocket exhaust mostly exist in the mixing layer of supersonic jet flows. This tends to reduce the intensity of shocks existing in the jet, responding to the variation of thermal parameters.     

A comparison of ionosonde measured foF2 and IRI-2016 predictions over China

A comparison of the ionospheric F-region critical frequency (foF2) between ionosonde measurements and IRI-2016 predictions is studied over China during the period from January 2008 to October 2016. Four stations are selected, and the latitude coverage starts at 49.4°N and ends at 23.2°N with a sequential latitude interval of about 10°, the corresponding geomagnetic latitudes are from 39.5°N to 13.2°N. The results show that the variability of the observed foF2 versus latitudes, seasons, local time and levels of solar activity could be well reproduced by IRI-2016. However, the daily lowest value of foF2 from the IRI-2016 prediction occurs earlier than that from the ionosonde. Around the sunrise, the IRI-2016 prediction shows a very sharp rise and grows much faster than the observed foF2 in every month. The foF2 difference between the two options (URSI and CCIR) in IRI-2016 increases as the F10.7 index decreases. During 2008–2009, the annual average deviations of URSI and CCIR range from ?5% to ?10% and from 5% to ?5%, respectively. Generally, the CCIR performs better than URSI during postsunset under low solar activity or in Equatorial Ionization Anomaly (EIA) region over China, while it shows no large difference in performance with URSI in other locations or for other time.     

信息战及其对机载计算机发展的影响

机载计算机系统是飞机航空电子系统的核心部件，它在信息战环境下的作战能力，直接决定了飞机在信息战中的生存能力和任务成功率。本文介绍了信息战的概念及特点，信息战对机载计算机系统的主要攻击形式，提出了机载计算机系统在现代信息战环境下必须加以考虑的几项关键技术。     

The morphology and velocity field of the large flare on the solar disc on July 14, 1980

The active region morphology and the features of solar radio bursts and sight-line velocity distribution of a flare of Importance 3B on the solar disc (AR 2562) on 1980 July 14 are introduced in this article.