THE RESEARCH OF INCREASING LIFT ANDREDUCING DRAG FOR WING-TIP SAILS

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Thermal cyclotron radiation from a hot coronal loop with helical magnetic field

The spectral and polarization properties of thermal cyclotron radio emission from a hot coronal loop with a current along the axis are computed. The magnetic field is supposed to have a component along the loop axis as well as a poloidal part due to the current, both components being of comparable magnitude. In this specific configuration a helical magnetic field is present with a remarkable minimum of its absolute value along the loop axis and a maximum at its periphery. The presence of one or two maxima of magnetic field value along the line of sight results in increasing optical thickness of the gyroresonance layers at appropriate frequencies in the microwave band and, therefore, in enhanced radio emission at those harmonics which are optically thin (for example,s=4). These cannot be observed in models with the commonly employed magnetic field configuration (longitudinal along the loop axis).We show that the frequency spectrum of thermal cyclotron radiation from a hot coronal loop with a helical magnetic field differs from that of the standards-component source (with smooth frequency characteristics and polarization corresponding toe-mode) in that plenty of fine structures (line-like features and cut-offs) are present and theo-mode is prevalent in some frequency intervals. The enhanced radio emission at high harmonics and the complicated form of frequency spectrum in the model considered imply that some microwave sources, which are poorly explained in traditional models of solar active regions, may be associated with helical magnetic fields in hot coronal loops. Computations allow one to indicate spectral and polarizational peculiarities of local sources testifying to the presence of a helical magnetic field.     

Dissipation of magnetic fields in active galactic nuclei

A model for the emission processes causing rapid variability (less than one day) in active galactic nuclei is developed. Relativistic electron beams escape from reconnection sheets in coronae of accretion disks and excite plasma turbulence with a typical frequency , which depends on the electron number densityn (see also the contribution by R. van Oss). The finite lengths of different beams emerging from different reconnection sheets allows that the waves arecoherently scattered to frequencies ²_pe. For Lorentz factors 10³ and densities typical for disk coronaen10⁶ cm ^–3 (derived from iron line observations) one easily reaches the optical, frequency range. The time scale of the variability is then caused by the relaxation of the electron beams. Likewise, this model explains the very rapid variability in the X-ray (less than 10 minutes) by changing the parameters slightly. According to this scenario the higher the variable frequency is, the closer to the central black hole it should originate.     

热结构动力优化设计

 考虑温度沿飞行器表面的分布及材料物性系数随温度的变化,按Ｋｕｈｎ－Ｔｕｃｋｅｒ条件建立迭代式,研究具有频率约束、振型节点约束以及变量上、下限约束的热结构动力优化设计。算例讨论了前３阶固有特性及最小目标随温度场的变化规律,证实本方法有效、可行。     

数据库的工程界面

 系统地论述了数据库的工程界面、数据库管理系统、程序设计语言三者之间的层次关系。以ＳＴＥＰ标准的ＳＤＡＩ（ＳｔａｎｄａｒｄＤａｔａＡｃｃｅｓｓｌｎｔｅｒｆａｅｅ）作为数据库工程界面的具体例子,详细地论述了它向ＯＤＢＭＳ及ＲＤＢＭＳ的映射。对于向ＲＤＢＭＳ的映射,提出了“知子女联系”向“知子女联系”的映射策略,为简化映射算法、提高系统效率提供了一种选择。     

跨声速翼型多目标优化设计方法

本文通过采用多目标分级优化方法并基于求解全速势方程的跨声速粘流翼型计算方法，研究发展了一种多参数、多约束和多目标的跨声速翼型数值优化设计方法，应用该方法可以从普通低速翼型和超临界民办型出发通过多目标优化后得到在跨声速区的多个马赫数下阻力系数最小化的翼型几何外形，设计实践表明，该方法具有收敛快，调用目标函数次数少等优点。     

航空发动机燃烧室进行间断喷油的试验研究

 在各种飞行条件下,航空发动机工况的改变是靠供油量的改变来实现的。而供油量的改变则是由于改变了供油压力。当喷嘴面积和流量系数不变的条件下,向燃烧室的喷油量与喷油压差成平方关系。由于飞机的飞行条件变化很大,喷油压力必将发生很大的变化。喷油压力是燃油在燃烧室里雾化的决定因素之一。当喷射压力低时,燃油的雾化质量不好,会导致燃烧效率的下降。     

铝合金锻件重复淬火保温时间对组织性能的影响

分析了铝合金锻件重复淬火保温时间的长短及其组织性能的影响情况。根据大量的试验数据,证实了重复淬火保温时间及时效保温时间的长短对锻件性能的直接影响,并以此确定了合理的工艺参数。     

喷管内缝隙流场与热环境数值模拟研究

用有限元素法数值模拟了固体火箭发动机喷管内缝隙的流场和热环境。采用非结构的高分辨率的有限元离散格式,计算了不同攻角和不同Ｍａ数的缝隙内压力分布和气动加热,分析了缝隙内流场和热环境特性,数值结果与风洞实验结果符合很好。     

飞船返回舱跨声速全局稳定性研究

根据国内外在飞船返咽舱这类短钝飞行器的亚、跨声速风洞试验中都发现了极限环振动形态这一问题,利用全局稳定性分析和数字仿真方法,研究了返回舱在跨声速和高亚声带飞行时的动稳定性,得到与风洞试验类似的结果,即返回舱处于极限环振动形态。因此,在返回舱再入亚、跨声这飞行段,为保证飞行安全,采用有效和可靠的姿态控制系统来控制和减缓动不稳定影响是必需的。