Calculation of the transonic dip of airfoils using viscous-inviscid aerodynamic interaction method

A numerical procedure for the calculation of the transonic dip of airfoils in the time domain is presented. A viscous-inviscid aerodynamic interaction method is taken to calculate the unsteady aerodynamic loads. In the present case the integral boundary layer equations are coupled with the Transonic Small Disturbance (TSD) Potential Equation. The coupling between structural motion and aerodynamic loads is carried out using State Space equation. It is solved by State Transition Matrix technique. Results are presented for NACA 64A010 and NLR 7301 airfoils with structural data from Isogai and DLR, respectively. Comparisons show good agreement with other numerical results. Certain deviations of experimental data taken from literature need more insight in the detailed test conditions.     

EUROPEAN NETWORK FOR THE NUMERICAL SIMULATION OF SPACE PLASMAS

The Cluster mission of the European Space Agency (ESA) will allow, for the first time three-dimensional measurements in key regions of the Earth's magnetosphere to be carried out. The European Numerical Simulation Network (ENSN) aims at providing a theoretical support to the mission. We describe the achievements of the ENSN during its first period of activity 1991–1994, during which the network was funded by the European Union. In particular, the ENSN has set up (i) thematic Working Groups on the prime scientific goals of the mission, (ii) a code development Working Group to develop numerical simulation codes specifically adapted to studying magnetospheric boundaries and the corresponding scale mixing, and (iii) software models of Cluster instruments to test in a numerical simulation what the set of four instruments will measure.     

三维极小脱靶量与极小能量综合最优控制律研究与仿真

根据空间平台拦截器与目标的相对运动方程,基于线性系统最优控制理论提出了一种综合三维极小脱靶量与极小能量的最优控制律。给出了最优推力大小与方向控制,以及最优过渡时间和关机时刻确定的模型。仿真结果表明:该最优控制律控制精度高,易于工程实现。     

空间能量粒子探测方法研究

阐述了空间能量粒子探测的原理和方法。介绍了国外在能量粒子探测方面所采用的半导体望远镜测量法、电场加速法、磁偏转法等方法，分析了它们各自的优缺点。就制约能量粒子探测技术发展的关键因素进行了讨论。并以此为基础，结合我国实际情况提出了一种新的探测方法。     

对“ZY-1”FM1整星热平衡、热真空试验中有效载荷被污染情况的分析

介绍了卫星在热平衡试验后所发现的有效载荷的污染情况,通过对污染提取物的分析和试验设备的再次污染监测,找出了污染源,并对以后的防污染工作提供了借鉴.     

大型空间模拟器真空测量的自动化

介绍了大型空间模拟器真空测量自动化的实施和特点,以及真空度的描述方法,对真空测量自动化的进一步发展提出了设想。     

抗空间碎片碰撞穿透的航天器加强防护板设计

文章描述了以整体薄护罩和等效重量波纹薄护罩制作的双层板结构系统穿孔阻力的研究结果。指出如果以等效重量波纹缓冲器代替整体缓冲器可以显著地增加穿孔防护能力。针对在倾斜超高速碰撞事件中跳飞碎片的产生,波纹薄护罩的波纹参数可以用减少势的方法优化。     

Progress in space weather predictions and applications

The methods of today’s predictions of space weather and effects are so much more advanced and yesterday’s statistical methods are now replaced by integrated knowledge-based neuro-computing models and MHD methods. Within the ESA Space Weather Programme Study a real-time forecast service has been developed for space weather and effects. This prototype is now being implemented for specific users. Today’s applications are not only so many more but also so much more advanced and user-oriented. A scientist needs real-time predictions of a global index as input for an MHD model calculating the radiation dose for EVAs. A power company system operator needs a prediction of the local value of a geomagnetically induced current. A science tourist needs to know whether or not aurora will occur. Soon we might even be able to predict the tropospheric climate changes and weather caused by the space weather.     

航天火工装置推力测量的干扰分析

航天火工装置种类很多,性能各异。文章仅对广泛使用的弹射器和解锁器类火工装置的推力测量系统进行论述,分析测量过程中的干扰环节,说明不同干扰类型对测量结果的影响。并提出测试改进建议。     

航天火工装置推力测量的干扰分析

航天火工装置种类很多，性能各异。文章仅对广泛使用的弹射器和解锁器类火工装置的推力测量系统进行论述，分析测量过程中的干扰环节，说明不同干扰类型对测量结果的影响。并提出测试改进建议。