可压缩轴对称射流流场近区的数值模拟

采用高精度差分方法对二维轴对称可压缩射流流场进行了数值模拟,研究了大尺度涡结构的形成和发展过程及其在射流雪展过程中的作用,计算结果显示了射流失稳后首先出现Ｋｅｌｖｉｎ－Ｈｅｌｍｈｏｌｔｚ非稳定特征,之后向下游发展的过程中, 一笥效应的增长导致涡的配对和对并;指出射流场中压力波动的分布是大尺度涡结构分布的直接结果。     

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。     

变化磁场产生涡旋电场的一般形式

本文中引入矢量电势以给出变化磁场产生涡旋电场的一般表达式以及二维情形中的形式．并用来对熟知的圆柱形磁场分布作了计算和讨论     

基于光楔阵列产生光学涡旋阵列的研究

在研究光楔衍射法产生单涡旋的基础上,基于长条形光楔阵列,提出了利用光束阵列衍射产生涡旋阵列的方法.该方法要求光束阵列在平行于光楔边缘方向上的光束间距等于光束直径的整数倍.利用超精密机床采用一体化加工法加工了光楔阵列元件,验证了该方法的可行性.利用空间光调制器快速灵活调整光束阵列的优点,搭建了借助空间光调制器加载达曼光栅衍射产生所需光束阵列的实验光学系统.针对光束阵列与光楔阵列的匹配问题,研究了达曼光栅掩模图基本单元对光束阵列的调控,获得了可调结构的光束阵列.实验产生了拓扑荷一致的光学涡旋阵列,与仿真结果相一致,证明所提方法的有效性.     

谐振子势与高斯势联合势阱中玻色爱因斯坦凝聚体的巨涡旋态

研究谐振子势与高斯势联合势阱中玻色爱因斯坦凝聚体的基态。发现凝聚体形成巨涡旋时,其涡旋个数等于平均角动量,且凝聚体密度分布和角动量密度分布相同,进而得到凝聚体形成巨涡旋时所处基态是角动量的本征态。发现势阱从各向同性的环形势阱逐渐变为各向异性的环形势阱的过程中,凝聚体的平均角动量与涡旋个数之比先由1平缓下降,然后迅速下降,最后保持在0.5附近。同时给出凝聚体密度分布和角动量分布的特征,并作出相应解释。     

High efficiency and broad bandwidth terahertz vortex beam generation based on ultra-thin transmission Pancharatnam–Berry metasurfaces

The terahertz(THz) vortex beam generators are designed and theoretically investigated based on single-layer ultra-thin transmission metasurfaces. Noncontinuous phase changes of metasurfaces are obtained by utilizing Pancharatnam–Berry phase elements, which possess different rotation angles and are arranged on two concentric rings centered on the origin.The circularly polarized incident THz beam could be turned into a cross-polarization transmission wave, and the orbital angular momentum(OAM) varies in value by lh. The l values change from ±1 to ±5, and the maximal cross-polarization conversion efficiency that could be achieved is 23%, which nearly reaches the theoretical limit of a single-layer structure.The frequency range of the designed vortex generator is from 1.2 THz to 1.9 THz, and the generated THz vortex beam could keep a high fidelity in the operating bandwidth. The propagation behavior of the emerged THz vortex beam is analyzed in detail. Our work offers a novel way of designing ultra-thin and single-layer vortex beam generators, which have low process complexity, high conversion efficiency and broad bandwidth.     

轴流压气机时尖泄漏涡的时均流动

用三维激光多普勒测速系统测量研究低速大尺寸单级压气机设计状态转子内尖区流场．结果表明，泄漏流在气流一进入转子叶片通道就开始发生，发生于前半弦长，其诱导形成的泄漏涡约在30％弦长处达到最强，随后逐渐衰减，其涡核顺下游慢慢向压力面方向和低时高方向移动，涡核在转子出口移至通道中部．泄漏涡影响区域沿流向逐渐扩大，并向压力面方向和低叶高方向移动．设计状态叶尖泄漏涡在转子尖区流动中起主要作用，是造成尖部流动阻塞的主要因素．     

Dynamics and formation of vortices collapsed from ring dark solitons in a two-dimensional spin–orbit coupled Bose–Einstein condensate

We consider the dynamics and formation of vortices from ring dark solitons in a two-dimensional Bose–Einstein condensate with the Rashba spin–orbit coupling based on the time-dependent coupled Gross–Pitaevskii equation. Compared with previous results, the system exhibits complex dynamical behaviors in the presence of the spin–orbit coupling. With the modulation of the spin–orbit coupling, not only the lifetime of ring dark solitons is greatly prolonged, but also their attenuation kinetics is significantly affected. For two shallow ring dark solitons with the equal strength of the spin–orbit coupling, the radius of ring dark solitons increases to a maximum value over time and then shrinks into a minimum value. Due to the effect of the snake instability, ring dark solitons split into a series of ring-like clusters of vortex pairs, which perform complex oscillations. This indicates that the system is strongly dependent on the presence of the spin–orbit coupling. Furthermore, the effect of different initial modulation depths on the dynamics of ring dark solitons is investigated.     

Interaction Mechanism and Loss Analysis of Mixing between Film Cooling Jet and Passage Vortex

The interaction between the film-cooling jet and vortex structures in the turbine passage plays an important role in the endwall cooling design. In this study, a simplified topology of a blunt body with a half-cylinder is introduced to simulate the formation of the leading-edge horseshoe vortex, where similarity compared with that in the turbine cascade is satisfied. The shaped cooling hole is located in the passage. With this specially designed model, the interaction mechanism between the cooling jet and the passage vortex can therefore be separated from the crossflow and the pressure gradient, which also affect the cooling jet. The loss-analysis method based on the entropy generation rate is introduced, which locates where losses of the cooling capacity occur and reveals the underlying mechanism during the mixing process. Results show that the cooling performance is sensitive to the hole location. The injection/passage vortex interaction can help enhance the coolant lateral coverage, thus improving the cooling performance when the hole is located at the downwash region. The coolant is able to conserve its structure in that, during the interaction process, the kidney vortex with the positive rotating direction can survive with the negative-rotating passage vortex, and the mixture is suppressed. However, the larger-scale passage vortex eats the negative leg of the kidney vortices when the cooling hole is at the upwash region. As a result, the coolant is fully entrained into the main flow. Changes in the blowing ratio alter the overall cooling effectiveness but have a negligible effect on the interaction mechanism. The optimum blowing ratio increases when the hole is located at the downwash region.     

60°三角翼前缘涡破裂及其控制实验研究

本文应用流动显示技术对矢量差动喷流情况下60°三角翼前缘涡破裂特性进行了实验研究,结果表明矢量差动喷流可以有效地控制前缘涡的破裂位置,且整个流场主要受喷流速度大的喷流的影响,该侧前缘涡的破裂位置随喷流速度的增大向下游发展,而另一侧前缘涡的破裂则提前发生;另外,在喷流速度差一定的情况下,喷流速度越小,对前缘涡的控制作用越明显．