27-day variation in solar-terrestrial parameters: Global characteristics and an origin based approach of the signals

The Earth and the near interplanetary medium are affected by the Sun in different ways. Those processes generated in the Sun that induce perturbations into the Magnetosphere-Ionosphere system are called geoeffective processes and show a wide range of temporal variations, like the 11-year solar cycle (long term variations), the variation of ～27?days (recurrent variations), solar storms enduring for some days, particle acceleration events lasting for some hours, etc.In this article, the periodicity of ～27?days associated with the solar synodic rotation period is investigated. The work is mainly focused on studying the resulting 27-day periodic signal in the magnetic activity, by the analysis of the horizontal component of the magnetic field registered on a set of 103 magnetic observatories distributed around the world. For this a new method to isolate the periodicity of interest has been developed consisting of two main steps: the first one consists of removing the linear trend corresponding to every calendar year from the data series, and the second one of removing from the resulting series a smoothed version of it obtained by applying a 30-day moving average. The result at the end of this process is a data series in which all the signal with periods larger than 30?days are canceled.The most important characteristics observed in the resulting signals are two main amplitude modulations: the first and most prominent related to the 11-year solar cycle and the second one with a semiannual pattern. In addition, the amplitude of the signal shows a dependence on the geomagnetic latitude of the observatory with a significant discontinuity at approx. ±60°.The processing scheme was also applied to other parameters that are widely used to characterize the energy transfer from the Sun to the Earth: F10.7 and Mg II indices and the ionospheric vertical total electron content (vTEC) were considered for radiative interactions; and the solar wind velocity for the non-radiative interactions between the solar wind and the magnetosphere. The 27-day signal obtained in the magnetic activity was compared with the signals found in the other parameters resulting in a series of cross-correlations curves with maximum correlation between 3 and 5?days of delays for the radiative and between 0 and 1?days of delay for the non-radiative parameters. This result supports the idea that the physical process responsible for the 27-day signal in the magnetic activity is related to the solar wind and not to the solar electromagnetic radiation.     

考虑辐射的化学平衡流驻点线解

本文用数值方法求解了化学平衡的高超声速粘性激波层驻点线流场。考虑了辐射和质量引射对流场的影响。辐射模型采用线和连续谱模型。文中讨论了引射率、头部半径、来流速度对壁面传热的影响。与有关文献结果比较表明,本文的方法是可行的。     

微重力科学与应用研究（上）

空间微重力环境的独特物理现象对航天器各系统均产生无法回避的影响，在型号研制中正确计入微重力效应是航天事业发展中的一个重要研究领域。在现阶段，航天器发动机再启动相关的微重力研究以及载人航天防火安全相关的微重力研究应当引起人们的高度重视。随航天事业的发展，微重力效应问题日益会严重起来（结构动力学、耦合动力学、多相流温控、低重星球场着陆撞击……），进行深入广泛的微重力效应研究对保证航天器飞行任务完成有着不应忽视的作用     

论贾谊的教育思想

贾谊是我国古代比较系统地提出教育思想的人之一。他的教学内容以儒家礼教为中心，以道德教育为目标，从而建构了他的教育思想的基本框架。他首倡胎教，他总结的一些经验和理论与现代的胎教思想不谋而合。他强调环境对教育的重大影响，认为良好的环境有利于提高品德，增长学识。在教与学这个矛盾中，他强调教师的积极主导作用，并明确指出了教师的职责和任务。     

Stellar infrared astronomy with EDISON

In this review the IR emission from circumstellar material is discussed, both of ionized gas and dust grains, and the astrophysical information that can be extracted from such observations. Some emphasis is placed on the possibilities of stellar IR astronomy using a large space-borne telescope, especially with respect to the much better spatial and spectral resolution of such a telescope compared to the current generation of ground-based and space IR telescopes.     

基于LabVIEW设计曲线拟合仪

基于LabVIEW图形化编程环境和软件分析库函数设计的曲线拟合仪，界面友好，功能齐全，操作简便，在科学研究和工程应用中具有较强的实用价值。文中简要介绍利用NI虚拟仪器技术设计曲线拟合仪的方法，给出软件设计思想与实现方案，对主要软件功能模块进行了分析。     

强辐射条件下应变测量的抗干扰技术研究

文章从动力学结构分析应变测量的基本原理入手,着重介绍了国防高科技试验中,在强辐射、强电磁脉冲干扰环境条件下,为保证应变测量的实现,经模拟试验研究,在应变测量时采用了一系列抗干扰技术措施,包括特殊环境条件下所用元器件材料的选择,传感应变计安装方式,组桥接线方式,密封屏蔽等技术。并介绍了这些技术措施在某试验现场应变测试试验中的应用概况.     

星载遥感器在模拟空间环境中辐射定标设备研制

文章简述了星载遥感器辐射定标设备的研制过程及其在模拟空间环境中的调试过程,试验证明了该设备设计的合理性。     

弹道靶红外辐射测量

为深入认识再入物理现象 ,在弹道靶上做了模型头部和近尾流红外辐射测量。发射器为 1 4.5mm口径的二级轻气炮 ,模型为1 0mm的球 ,材料为聚碳酸酯和铝 ,模型发射速度 4～6km/s,使用红外InSb探测器测量波长 3～ 5 .4μm的红外辐射 ,靶室压力 5 .32kPa。实验中使用光电法测量模型速度 ,两站阴影照相进行模型姿态监测和速度核实。实验结果表明 :球模型的红外辐射强度强烈依赖于模型材料和模型飞行速度。对不同材料模型头部和尾流部辐射强度的定性比较说明由于低温材料烧蚀产物的存在 ,极大地增强了头部和近尾流区的辐射强度 ,而且延长了尾流辐射长度     

低地球轨道环境原子氧对航天器表面材料聚酰亚胺作用的数值模拟

在建立数学物理模型的基础上，对氏地球轨道环境和地面实验环境下，有无保护层的聚酰亚胺所受原子氧冲蚀作用进行了进行了成功的数值模拟，获得了具有工程应用价值的数值计算结果，并讨论了数学物理模型中各参数对基蚀曲线形状的影响。从数值模拟结果和美国太空实验结果的比较可以看出，本文数据模拟的结果是正确的。该项工作对航天器的设计具有重要指导意义。