空间任意形状凸面的轨道空间外热流计算方法

采用蒙特卡罗（ＭｏｎｔｅＣａｒｌｏ）方法，进行了平板、半球面、抛物面的地球反照角系数和地球红外角系数计算，通过与文献数据的比较，证明了由此方法所编程序的可靠性和实用性。利用这种方法，可以计算空间任意形状凸表面的轨道空间外热流。     

战争中毁灭的人生——邓一光小说《远离稼穑》人物分析

在战争中个人要承受生命中怎样无法言说的沉重,作家邓一光通过他的中篇小说《远离稼穑》进行有益的探索,刻画"我的四爷"这样一个有过三次特殊被俘经历的人物形象,表现作家以勇气和胆识对战争文学题材的开掘与对角度的拓展所做出的努力。     

螺旋相位板生成涡旋电磁波仿真研究

涡旋电磁波的产生方式有多种,使用涡旋相位板即为其中重要的一种方式。该文对螺旋相位板产生涡旋电磁波的情况进行了仿真.通过仿真。给出了在喇叭天线口面上覆盖螺旋相位板时生成的涡旋电磁波的幅度相位分布。     

网格拓扑对DLR-F6构型数值模拟的影响

基于TRIP3.0软件平台和多块结构网格技术,开展了控制方程和网格拓扑等因素对DLR-F6构型数值模拟的影响研究。数值计算采用与试验相同的参数,采用了RANS/TLNS方程,生成了O型和H型2种拓扑的粗、中、细网格进行模拟。分别从气动特性、压力系数分布曲线和表面流态3个方面对结果进行分析。通过与试验数据的对比表明,在模拟小分离流动时,采用H型拓扑网格和RANS方程模型,获得的计算结果会更为准确。     

The use of Gaussian equations of motions of a satellite for local gravity anomaly recovery

The orbital elements of a low Earth orbiting satellite and their velocities can be used for local determination of gravity anomaly. The important issue is to find direct relations among the anomalies and these parameters. Here, a primary theoretical study is presented for this purpose. The Gaussian equations of motion of a satellite are used to develop integral formulas for recovering the gravity anomalies. The behaviour of kernels of the integrals are investigated for a two-month simulated orbit similar to that of the Gravity field and steady-state ocean circulation explorer (GOCE) mission over Fennoscandia. Numerical investigations show that the integral formulas have neither isotropic nor well-behaved kernels. In such a case, gravity anomaly recovery is not successful due to large spatial truncation error of the integral formulas. Reformulation of the problem by combining the orbital elements and their velocities leads to an integral with a well-behaved kernel which is suitable for our purpose. Also based on these combinations some general relations among the orbital elements and their velocities are obtained which can be used for validation of orbital parameters and their velocities.     

多任务在轨服务模块化智能航天器技术研究

首先介绍了在轨服务技术的分类及国内外近期研究进展,结合各国已开展项目的验证情况,分析了在轨服务模式、适应多任务在轨服务航天器的发展思路。为适应卫星发射和在轨服务的任务需要,提出了多任务服务航天器的方案设想,以期降低在轨服务操作的难度,提升在轨服务系统执行多任务的能力。最后初步分析了用于演示验证任务的服务航天器总体参数及任务规划。     

Characterization of the cataloged Fengyun-1C fragments and their long-term effect on the LEO environment

The intentional breakup of Fengyun-1C on 11 January 2007 created the most severe orbital debris cloud in history. The altitude where the event occurred was probably the worst location for a major breakup in the low Earth orbit (LEO) region, since it was already highly populated with operational satellites and debris generated from previous breakups. The addition of so many fragments not only poses a realistic threat to operational satellites in the region, but also increases the instability (i.e., collision cascade effect) of the debris population there.     

Dynamical evolution of high area-to-mass ratio debris released into GPS orbits

A large set of simulations, including all the relevant perturbations, was carried out to investigate the long-term dynamical evolution of fictitious high area-to-mass ratio (A/M) objects released, with a negligible velocity variation, in each of the six orbital planes used by Global Positioning System (GPS) satellites. As with similar objects discovered in near synchronous trajectories, long lifetime orbits, with mean motions of about 2 revolutions per day, were found possible for debris characterized by extremely high area-to-mass ratios. Often the lifetime exceeds 100 years up to A/M ∼ 45 m²/kg, decreasing rapidly to a few months above such a threshold. However, the details of the evolution, which are conditioned by the complex interplay of solar radiation pressure and geopotential plus luni-solar resonances, depend on the initial conditions. Different behaviors are thus possible. In any case, objects like those discovered in synchronous orbits, with A/M as high as 20–40 m²/kg, could also survive in this orbital regime, with semi-major axes close to the semi-synchronous values, with maximum eccentricities between 0.3 and 0.7, and with significant orbit pole precessions (faster and wider for increasing values of A/M), leading to inclinations between 30° and more than 90°.     

双组尾翼弹气动特性计算与分析

本文根据双组尾翼弹的外形特点，选用了代数网格生成方法，通过求角N－S方程，对其气动特性进行了数值计算，并对其计算结果进行了分析。由计算结果可知，此种弹的双尾翼可以为其提供一定的转速和升力，提高其静稳定性。并且此种弹已经用于型号设计。     

进入中、韩两国的「日本製漢語」研究

「日本製漢語」是日本创造的汉字词,现已成为汉语和韩语的重要组成部分。分析了「日本製漢語」产生的原因和过程,探讨了「日本製漢語」进入中国和韩国的历史、政治和文化背景,并以「同形同義語」、「同形類義語」、「同形？義語」三个类型的「日本製漢語」,从数量、语义比较研究了它们在汉语和韩语中的差异及不同用法。