高温超导体Josephson阵列在磁场中的微波响应与磁通涡旋激发

本文从分析相变电阻率 ρP 和磁通蠕动电阻率 ρF 出发 ,指出当T小于某一温度T0 时 ,ρF>ρP,而当T >T0 时 ,ρF 远小于 ρP,并进一步分析了 ρF 与 ρP 随温度的变化率分布图 ,得出磁通蠕动电阻率 ρF 随温度的变化率分布图跟微波响应曲线具有相似的分布特征 ,结果表明 :高温超导体的非平衡微波响应机制可能与磁通涡旋的激发有关 .     

部分相干双曲正弦-Gauss涡旋光束叠加形成的合成相干涡旋在非 Kolmogorov 大气湍流中的动态演化

一些实验表明, 实际大气会偏离理想Kolmogorov模型. 本文基于广义Huygens-Fresnel原理和Toselli等提出的非Kolmogorov湍流模型, 推导出部分相干双曲正弦-Gauss (HSG)涡旋光束通过非Kolmogorov大气湍流的解析传输公式, 并用以对两束部分相干HSG涡旋光束相干叠加和非相干叠加形成的合成相干涡旋在非Kolmogorov大气湍流中的动态演化进行了研究. 结果表明, 合成光束平均光强的演化过程与非Kolmogorov湍流的广义指数α, 源平面上叠加涡旋光束拓扑电荷的符号, 以及叠加方式有关. 合成相干涡旋在非Kolmogorov大气湍流中传输时会出现移动、产生和湮灭. 广义指数α, 拓扑电荷符号, 以及叠加方式都会影响其演化行为. 最后, 将本文所得结果与相关文献做了比较.     

STUDY ON THE FUEL AIR MIXING INDUCED BY A SHOCK WAVE PROPAGATING INTO A H_2-AIR INTERFACE

ＩｎｔｒｏｄｕｃｔｉｏｎＴｈｅｆｕｅｌａｉｒｍｉｘｉｎｇｉｎａｓｈｅａｒｌａｙｅｒｆｌｏｗｉｓａｎｉｍｐｏｒｔａｎｔｐｒｏｂｌｅｍｉｎｓｔｕｄｙｉｎｇｃｏｍｐｒｅｓｓｉｂｌｅｆｌｏｗａｎｄｓｕｐｅｒｓｏｎｉｃｃｏｍｂｕｓｔｉｏｎ ,ｓｕｃｈａｓｆｕｅｌｄｉｆｆｕｓｉｏｎａｎｄｍｉｘｉｎｇｉｎａＳｃｒａｍｊｅｔ[1].Ｒｏｓｈｋｏ[2 ]ｓｔｕｄｉｅｄｅｘｐｅｒｉｍｅｎｔａｌｌｙｔｈｅｐｈｅｎｏｍｅｎｏｎｏｆｆｕｅｌａｉｒｍｉｘｉｎｇｉｎａｓｕｂｓｏｎｉｃｓｈｅａｒｆｌｏｗａｎｄｆｏｕｎｄｌａｒｇｅ ,ｃｏｈ…     

点涡动力系统的Lyapunov指数

平面上理想流体的三点涡系统是可积的Hamilton系统, 但其运动仍然相当复杂, 这给研究被动微粒在三点涡系统中运动带来了很大的困难. 着眼于点涡系统的被动微粒对初始小扰动的稳定性, 通过Oseledec定理定义被动微粒的Lyapunov指数, 给出了点涡系统中被动微粒稳定性的定量刻画. 同时, 由Hamilton系统的保体积性质得到的关于Lyapunov指数的简洁表达式, 避免了计算的繁琐. 利用这个定义, 点涡系的瞬时流场可以被划分成若干区域, 被动微粒的混沌运动只能在近涡的特定区域出现.      

非光滑叶片对叶栅流道内通道涡影响的实验研究

在低速平面叶栅风洞中对光滑叶片叶栅及三种非光滑叶片叶栅进行了实验研究,以研究 与光滑叶片相比,非光滑叶片对叶栅流道内通道涡发展变化的影响。实验结果表明,与光滑叶片相 比,非光滑叶片对叶栅流道内的通道涡有明显的影响,通道涡的位置沿节距方向移向流道中心处, 沿叶高方向不变,通道涡的强度有所减弱。分析了非光滑叶片的影响原因。     

Experimental observation of dust circulation in unmagnetized cogenerated dusty plasma

The vortex motion of a dust cloud was experimentally observed in unmagnetized cogenerated dusty plasma in different experimental parameters. Particle image velocimetry analysis demonstrated that several vortex zones exist in the dust cloud at relatively low pressures (0.06 mbar (or 6 Pa)–0.08 mbar (or 8 Pa)) and low discharge voltages (peak‐to‐peak voltage 540–560 V), whereas in relatively high pressure (0.4 mbar (or 40 Pa)–0.7 mbar (or 70 Pa)) and high discharge voltage (peak‐to‐peak voltage 690–740 V), dust vortices formed in dense dust cloud with background plasma fluctuation.     

有限平板绕流的数值模拟

本文用涡团法模拟了有限平板的绕流问题,计算出一个长度为1的无穷薄平板在静止的流体中突然起动并作匀速运动的周围流场的变化情况。方法上,用保角变换解决了在涡团法中遇到的一个拉普拉斯方程,并对变换中的奇点作了特殊处理,最后得到一个与已有的实验结果完全吻合的周期性数值解。     

绒毛控制圆柱涡激振动的风洞试验研究

利用绒毛对圆柱涡激振动抑制进行了风洞试验研究。通过改变附属绒毛无因次长度L/D比(L为绒毛长度,D为圆柱外径),研究L/D分别为0.6、1.2和1.8的模型在约化速度2~40的范围内对弹性支撑大质量阻尼系数圆柱涡激振动的抑制作用。试验采用激光位移传感器采集圆柱的横向(Y)和顺流向(X)位移,并用烟线测流场以揭示流动控制机理。结果表明,三种无因次长度的绒毛对大质量阻尼系数圆柱的涡激振动都有显著的抑制作用,随着L/D的增加,圆柱Y向无因次位移及功率谱密度幅值减弱,多达73.5%的无因次位移被抑制;且随着L/D的增加,圆柱附属绒毛频率比远离原始圆柱频率比。绒毛改变了圆柱的边界层分离点位置、抑制了边界层的相互作用并改变尾涡结构,从而抑制振动。     

Further study on vortex shedding flow by a circular cylinder

In the present paper the mechanism involved in vortex shedding flows is investigated in detail. In the early stage of the unsteady separated flow the interaction between secondary vortices and primary vortices is quite strong. In the later stage of the flow, corresponding to the vortex shedding the recirculating flow region on each side of the aft body goes through such a cycle: growth-contraction-growth, the secondary separation occurs periodically rather than continuously. The reduction of circulation is taken into account in three cases with different decay factors to study its influence on the prediction of main flow characteristics. Results show that to simulate vortex shedding flow it is necessary to include the reduction of circulation to bring the calculated results into good agreement with experiments. An improved discrete vortex model is suggested in which both the secondary separation and the reduction are incorporated. The processes of vortex shedding, the forces prediction and other flow characteristics are given and some discussions are made. Porject is supported by National Natural Science Foundation of China.     

Regimes of vortex shedding from an in-line oscillating circular cylinder in the uniform flow

A finite volume method for the time dependent viscous incompressible flow around an in-line oscillating circular cylinder at Reynolds number of 200, 855 is presented in this paper. The Navier-Stokes equations in a finite volume form are solved with a moving grid system, based on a time dependent coordinate transformation. To investigate the vortex-shedding characteristics behind the circular cylinder and the effects of Reynolds number and other non-dimensional parameters such as reduced amplitude and reduced frequency， several numerical schemes have been tested with different amplitude and frequency close to Sto and a harmonic at each Reynolds number. Present numerical results indicate several types of vortex shedding mode which is known mainly depending on the reduced frequency and also the reduced amplitude, which is called synchronization or lock-on.