A statistical analysis of low frequency geomagnetic field pulsations at two Antarctic geomagnetic observatories in the polar cap region

The aim of this study is to investigate the characteristics of low frequency (∼0.5–5 mHz) geomagnetic field fluctuations as recorded at two Antarctic stations within the polar cap: the Italian observatory Mario Zucchelli Station (TNB) and the French–Italian observatory Dome C (DMC) in order to investigate the spatial extension and propagation characteristics of the phenomena observed at very high latitude. The stations have approximately the same geographic latitude, but a very different corrected geomagnetic latitude, being DMC close to the geomagnetic pole and TNB closer to the auroral oval.     

INVESTIGATION OF ACTIVE CONTROL FOR DYNAMIC STABILITY OF HELICOPTER ROTOR－BODY COUPLING

ＩＮＶＥＳＴＩＧＡＴＩＯＮ　ＯＦ　ＡＣＴＩＶＥ　ＣＯＮＴＲＯＬ　ＦＯＲ　ＤＹＮＡＭＩＣ　ＳＴＡＢＩＬＩＴＹ　ＯＦ　ＨＥＬＩＣＯＰＴＥＲ　ＲＯＴＯＲ－ＢＯＤＹ　ＣＯＵＰＬＩＮＧＬｉｎｇＡｉｍｉｎ（ＣｈｉｎｅｓｅＨｅｌｉｃｏｐｔｅｒＲｅｓｅａｒｃｈａｎｄ...     

Energy flux in the Earth's magnetosphere: Storm – substorm relationship

Three ways of the energy transfer in the Earth's magnetosphere are studied. The solar wind MHD generator is an unique energy source for all magnetospheric processes. Field-aligned currents directly transport the energy and momentum of the solar wind plasma to the Earth's ionosphere. The magnetospheric lobe and plasma sheet convection generated by the solar wind is another magnetospheric energy source. Plasma sheet particles and cold ionospheric polar wind ions are accelerated by convection electric field. After energetic particle precipitation into the upper atmosphere the solar wind energy is transferred into the ionosphere and atmosphere. This way of the energy transfer can include the tail lobe magnetic field energy storage connected with the increase of the tail current during the southward IMF. After that the magnetospheric substorm occurs. The model calculations of the magnetospheric energy give possibility to determine the ground state of the magnetosphere, and to calculate relative contributions of the tail current, ring current and field-aligned currents to the magnetospheric energy. The magnetospheric substorms and storms manifest that the permanent solar wind energy transfer ways are not enough for the covering of the solar wind energy input into the magnetosphere. Nonlinear explosive processes are necessary for the energy transmission into the ionosphere and atmosphere. For understanding a relation between substorm and storm it is necessary to take into account that they are the concurrent energy transferring ways. This revised version was published online in August 2006 with corrections to the Cover Date.     

后掠激波边界层干扰的有利影响

本文分析和对比了正激波和后掠激波/边界层干扰的机理,并用几个典型的算例说明了其差别.本文的结果指出,由于后掠的压力梯度方向垂直于激波,并且边界层内速度存在平行于激波的横向分量,会导致边界层内的速度分布形成空间"扭曲",可以阻止部分边界层进入激波后,并使穿过激波的部分边界层气流形成向两侧发散的趋势.这证明利用后掠激波/边界层干扰效应控制边界层是可行的.这也是实现近年来国内外兴起的"无隔道进气道"的关键机理之一.     

Characterization of component interactions in two-stage axial turbine

This study concerns the characterization of both the steady and unsteady flows and the analysis of stator/rotor interactions of a two-stage axial turbine. The predicted aerodynamic performances show noticeable differences when simulating the turbine stages simultaneously or separately. By considering the multi-blade per row and the scaling technique, the Computational fluid dynamics(CFD) produced better results concerning the effect of pitchwise positions between vanes and blades. The recorded pressure fluctuations exhibit a high unsteadiness characterized by a space–time periodicity described by a double Fourier decomposition. The Fast Fourier Transform FFT analysis of the static pressure fluctuations recorded at different interfaces reveals the existence of principal harmonics and their multiples, and each lobed structure of pressure wave corresponds to the number of vane/blade count. The potential effect is seen to propagate both upstream and downstream of each blade row and becomes accentuated at low mass flow rates. Between vanes and blades, the potential effect is seen to dominate the quasi totality of blade span, while downstream the blades this effect seems to dominate from hub to mid span. Near the shroud the prevailing effect is rather linked to the blade tip flow structure.     

在电离层飞行的航天器近尾迹内电子数密度渐近解

本文讨论了航天器近尾迹流场电子数密度分布,给出无碰撞假设下等离子体绕带电圆盘流动的近尾迹流场渐近解。用匹配渐近展开法求解实际可能现出的三种情形的电子数密度分布。所得的摄动解对近尾迹流动的理论和数值研究有指导意义。     

跨声速工况下流体诱发叶片振动研究

对同一跨声速风扇的非定常流场进行了跨声与亚声两种工况下的数值模拟.对两个工况下流场计算得到的转子叶片表面非定常气动激振力进行频谱分析,并对其进行对比分析,从而得到跨声工况下气动激振力特性.应用ANSYS软件的瞬态分析方法进行了叶片的强迫响应分析,对跨声和亚声两种工况下的叶片强迫响应进行对比分析,从而得到跨声工况下叶片强迫响应特性.      

突扩燃烧室湍流射流的相互作用及其对燃烧与混合的影响

本文应用κ－ε湍流模型和快速化学反应的守恒标量简化ＰＤＦ模型,对有中心射流和环状射流相互作用的突扩燃烧室内的湍流流动,混合与扩散燃烧进行了数值模拟。研究了环状射流与中心射流的速度比在较大范围内改变时突扩燃烧室内湍流回流流场的变化,揭示了较大的射流速度比对突扩燃烧室内湍流混合与燃烧的强化作用。     

流向入射涡与后翼相互作用分析

涡翼互作用现象影响航空运输编队飞行的效益和配对进近的安全。采用数值模拟方法,针对无入射涡影响的后翼以及稳定状态下的入射涡位于后翼3个典型展向位置共4种情况,研究入射涡与后翼的相互作用。对比分析了基于Q准则的三维涡量、不同流向位置的涡量,以及后翼吸力面静压系数、气动参数和滚转力矩系数等。研究结果表明:稳定状态下的入射涡在后翼外侧时,翼尖涡受上洗运动影响;在内侧时,受下洗运动影响。两种情况下,翼尖涡强度均受到抑制。入射涡越靠近后翼翼尖,后翼升力系数、升阻比、滚转力矩系数越大,且在其与后翼翼尖重合时都达到最大值。这一结果可为编队飞行和配对进近的前后机布局提供参考。     

超音速气流绕局部透气凹角流动的数值模拟

以具有压力分裂形式的简化Ｎ Ｓ方程为控制方程,数值模拟了超音速来流条件下的激波 边界层干扰被动控制（ｐａｓｓｉｖｅｃｏｎｔｒｏｌｏｆｓｈｏｃｋ ｂｏｕｎｄａｒｙｌａｙｅｒｉｎｔｅｒａｃｔｉｏｎ）。模拟是以预先给定激波前吹气和激波后吸气的流量来实现的。为了定性地确定吹气或吸气对激波 边界层干扰的影响,首先计算了单独吹气和单独吸气两种情况。数值计算时采用了多重扫描法对控制方程差分离散,以反映亚音速区压力对流场的椭圆性影响。