基于分布式仿真的导引头试验与评估技术研究

分析了未来导引头试验与评估的需求,提出了一种基于分布式仿真的导引头试验与评估系统的结构,分析了其关键技术。     

固体火箭发动机内弹道性能预示的一种方法

介绍一种在固体火箭发动机药型及其尺寸一定的条件下,利用发动机静止点火试验结果预示其内弹道性能的方法。利用这一方法,可以计算在概率条件下发动机的内弹道参数及总体参数的散布。     

A question raised from the observation of dynamic cusp formation: When and where does particle acceleration occur?

We present observations of a C9.4 flare on 2002 June 2 in EUV (TRACE) and X-rays (RHESSI). The multiwavelength data reveal: (1) the involvement of a quadrupole magnetic configuration; (2) loop expansion and ribbon motion in the pre-impulsive phase; (3) gradual formation of a new compact loop with a long cusp at the top during the impulsive phase of the flare; (4) appearance of a large, twisted loop above the cusp expanding outward immediately after the hard X-ray peak; and (5) X-ray emission observed only from the new compact loop and the cusp. In particular, the gradual formation of an EUV cusp feature is very clear. The observations also reveal the timing of the cusp formation and particle acceleration: most of the impulsive hard X-rays (>25 keV) were emitted before the cusp was seen. This suggests that fast reconnection occurred during the restructuring of the magnetic configuration, resulting in more efficient particle acceleration, while the reconnection slowed after the cusp was completely formed and the magnetic geometry was stabilized. This observation is consistent with the observations obtained with Yohkoh/Soft X-ray Telescope (SXT) that soft X-ray cusp structures only appear after the major impulsive energy release in solar flares. These observations have important implications for the modeling of magnetic reconnection and particle acceleration.     

计算机辅助喷丸工艺规程设计研究与应用

传统喷丸工艺规程的设计方法是由工艺人员根据他们从事工厂生产活动而积累起来的经验，以手工方式进行的，缺乏一致性，还存在着大量的重复劳动。计算机辅助喷丸工艺规程设计（ＳＰ－ＣＡＰＰ）是专门为从事喷丸工艺规程编制工作的技术人员所设计的计算机软件系统。它具有操作简便、功能强大、用户界面丰富多彩、容错性良好和高度自动化等特点，是使喷丸工艺规程设计工作高质量、高效率、集成化和规范化的有力工具。     

多目标翼型优化设计基因算法研究

本文把基因算法用于多目标翼型优化设计,针对基因算法的搜索原理和气功外形特点,提出了与之相适应的Ｂｅｚｉｅｒ曲线基因表达,构造了用于优化设计的适应度函数,发展了一种小种群演化方法。针对小种群基因算法中出现的近亲繁殖问题,提出了远亲配对策略、构造了自适应非均匀变异算子,提高了算法的收敛速度。文中最后给出了基于全位势方程求解程序的翼型重构反设计以及单目标和多目标翼型优化算例。     

电子束固化环氧树脂的引发和增长反应速率

对二苯基碘 鎓 六氟磷酸盐引发的环氧树脂电子束(EB)辐射固化反应动力学进行了研究,应用环氧树脂乙腈溶液推导出引发剂辐射分解速率常数和引发、增长反应速率.动力学研究结果表明,二苯基碘 鎓六氟磷酸盐引发剂经电子束辐射分解产生质子酸的过程是二级反应,在辐射反应过程中,环氧树脂体系的引发速率和增长速率分别迅速达到最大值后逐渐减小.      

跨声速风洞全模颤振试验技术

介绍了跨声速全模颤振试验的发展现状和存在的问题。探讨了全模颤振试验对风洞和支撑系统等试验设备的要求。对于风洞,主要从风洞洞体和流场等方面分析了进行颤振试验所需要具备的性能,并以中国空气动力研究与发展中心的2.4m跨声速风洞为例,介绍了进行颤振试验必须要采取的控制措施。对于支撑系统,则从模型运动自由度、支撑系统稳定性和支撑系统频率等方面的要求,阐述了设计支撑系统的困难,并简要分析了目前国内外发展的多种全模颤振支撑系统的结构原理及其优缺点。然后介绍了系统安全的保证措施,包括支撑系统稳定性分析、风洞紧急停车控制系统和模型保护装置等。最后根据飞行器发展的需求,探讨了今后需要完善和发展的几个主要问题。     

The Neupert effect and new RHESSI measures of thetotal energy in electrons accelerated in solar flares

It is believed that a large fraction of the total energy released in a solar flare goes initially into acceleratedelectrons. These electrons generate the observed hard X-ray bremsstrahlung as they lose most of their energy by coulomb collisions in the lower corona and chromosphere. Results from the Solar Maximum Mission showed that there may be even more energy in accelerated electrons with energies above 25 keV than in the soft X-ray emitting thermal plasma. If this is the case, it is difficult to understand why the Neupert Effect — the empirical result that for many flares the time integral of the hard X-ray emission closely matches the temporal variation of the soft X-ray emission — is not more clearly observed in many flares. From recent studies, it appears that the fraction of the released energy going into accelerated electrons is lower, on average, for smaller flares than for larger flares. Also, from relative timing differences, about 25% of all flares are inconsistent with the Neupert Effect. The Reuven Ramaty High Energy Solar Spectroscopic Imager (RHESSI) is uniquely capable of investigating the Neupert Effec since it covers soft X-rays down to 3 keV (when both attenuators are out of the field of view) and hard X-rays with keV energy resolution, arcsecond-class angular resolution, and sub-second time resolution. When combined with the anticipated observations from the Soft X-ray Imager on the next GOES satellite, these observations will provide us with the ability to track the Neupert Effect in space and time and learn more about the relation between plasma heating and particle acceleration. The early results from RHESSI show that the electron spectrum extends down to as low as 10 keV in many flares, thus increasing the total energy estimates of the accelerated electrons by an order of magnitude or more compared with the SMM values. This combined with the possible effects of filling factors smaller than unity for the soft X-ray plasma suggest that there is significantly more energy in nonthermal electrons than in the soft X-ray emitting plasma in many flares.     

先进飞机平台天线孔径综合的总体设计技术

电子信息系统的综合一体化是先进平台的典型特征,天线孔径综合将众多分立的天线单元/阵列进行整合,可显著地缩减平台天线数量,改善平台的气动和隐身性能。天线孔径综合需要满足小尺寸、高性能、低耦合等诸多要求,是射频综合系统的主要难点之一。以先进飞机平台为例,介绍天线孔径综合的总体设计技术,主要包括天线孔径综合的总体思路、电磁兼容性的考虑和典型天线样机的研制。     

带连续变弯度后缘操纵面机翼的动态失速减缓

主动偏转后缘操纵面可以减小翼型动态失速对气动特性产生的不利影响。研究连续变弯度后缘操纵面在减缓翼型动态失速方面的性能,利用CFD 结合动网格方法,计算NACA 0012 翼型在大幅度俯仰振荡时的非定常气动力;从减缓效果和能量需求两个方面,对比传统刚性操纵面和两种连续变弯度操纵面的动态失速减缓性能。结果表明：当后缘操纵面按正弦脉冲规律偏转时,可以推迟前缘涡的产生,加速后缘涡的发展,降低压力分布在后缘的峰值,进而减小动态失速时翼型的低头力矩极值;后缘操纵面的弯度构型会影响减缓效果,在相同的偏转策略下,弯度描述函数为2 阶多项式的连续变弯度操纵面的减缓效果最好,且能量需求最小。