二维圆柱层流绕流及其控制数值模拟

采用有限体积法求解二维N-S方程,通过改变时间、空间计算参数,对雷诺数100的二维圆柱非定常流场进行了数值模拟,将所得结果与实验数据以及已有的计算结果进行了对比.并对在尾部多个位置加入不同长度阻隔板控制流动的圆柱流场进行了考察.结果发现:在合适的位置放置阻隔板,可以有效抑制尾迹中涡脱落的形成.     

斜流式泵喷水推进器内部流动不稳定性分析

为了揭示斜流式泵喷水推进器的内部流动规律,利用多重参考系法,选用标准k-ε湍流模型和SIM-PLE算法,对不同工况下斜流式泵喷水推进器进行了数值模拟,分析了泵内部流动与其不稳定性之间的关系及叶轮叶片表面的压力分布规律.结果表明：扬程系数ψ与Q/Qbep曲线在流量为0.65Qbep～0.67Qbep工况下出现了正斜率（Q为工况点流量,Qbep为最佳设计工况点流量）,主要原因是导叶进口轮毂处的回流撞击叶轮出口流动,使其产生流动分离,最终形成旋涡,导致内部流动不稳定,从而使压力上升;在流量为0.65Qbep和0.85Qbep工况下,导叶内均出现回流,回流区域及回流速度随流量减小而增大.模拟分析说明斜流式泵喷水推进器在小流量工况下运行具有不稳定性.     

西南涡大气边界层结构的数值模拟Ⅱ:边界层物理量的数值分析

本文在计算分析了一个西南涡Ekman层流场特征的基础上,进一步对该西南涡边界层涡度、散度和垂直速度进行了数值分析,初步得出了西南涡在边界层内的垂直结构及物理量分布特征。     

基于时空特征融合的飞机尾涡识别

为了实现动态尾流缩减技术,减少进近阶段前机尾流对后机飞行安全的影响。依据相干激光雷达(coherent Doppler lidar, CDL)扫描风场循环周期性特点,提出一种基于时空特征融合的飞机尾涡识别模型。首先,CDL扫描生成的径向速度风场转换成序列输入和块输入。然后,双向长短时记忆(bidirectional long short-term memory, Bi-LSTM)网络用于提取序列输入的时间域特征,卷积神经网络(convolutional neural network, CNN)网络用于提取径向速度风场块输入的空间域特征。最后,将融合的时间域和空间域特征输入全连接层分类器,得到最终分类识别结果。实验团队在深圳宝安机场附近采集风场,并构建尾流数据集来验证所提得融合模型。结果表明：基于CNN和Bi-LSTM时空特征融合模型具有较好的分类性能,在尾涡识别上的准确率、召回率、F₁分数分别达到97.13%、97.50%、97.03%,且相比单一模型是一种更有效的识别方式,能够获得实时高效尾流预警。     

用于提高油田采收率的聚合物降解与防护

聚合物驱油是目前工业化应用程度最高的提高采收率三次采油方法,注入溶液的性能指标直接影响聚合物的增油效果,聚合物溶液的降解和防护已引起石油科技工作者的广泛关注。通过大量的室内实验和现场试验对聚合物驱油可能引起的机械降解、化学降解和生物降解进行了详细分析,对如何做好聚合物溶液降解的防护提出了可操作性的措施,在胜利油田应用后取得了预期的聚合物粘度保护效果,这对我国高含水油田聚合物驱油的广泛推广应用具有重要的现实意义。     

Diasteroselective Addition of Monoand Bis-Silylphosphines to Chiral Aldehydes

Abstract

The addition of silylphosphines to chiral aldehydes proceeds with high diastereoselectivity to give optically pure tertiary α -trimethylsiloxyalkylphosphines. The diastereomeric excesses of the addition products were achieved to 90–100%. The reaction of bis(trimethylsilyl)phenylphosphine with the acetonide of (R)-glyceraldehyde provides diastereomerically enriched tertiary bis(glyceryl)phosphines.     

Room Temperature Ionic Liquids in Asymmetric Hetero-Ene Type Reactions: Improving Organocatalyst Performance at Lower Temperatures

Room temperature ionic liquids (RTILs) have been widely used as (co)solvents in several catalytic processes modifying, in most of the cases, the catalyst activity and/or the selectivity for the studied reactions. However, there are just a few examples of their use in hydrogen bonding organocatalysis. In this paper, we show the positive effect of a set of imidazole-based ionic liquids ([bmim]BF₄ and [hmim]PF₆) in the enantioselective addition of formaldehyde tert-butylhydrazone to prochiral α-keto esters catalyzed by a sugar-based chiral thiourea. Reactions performed in the presence of low percentages of RTILs led to an increase of the catalyst activity, thereby making possible to work at lower temperatures. Thus, the chiral tert-butyl azomethyl tertiary alcohols could be obtained with moderate to good conversions and higher enantioselectivities for most of the studied substrates when using up to 30 vol% of [hmim]PF₆ as a cosolvent in processes performed in toluene.     

制约河北省农村第三产业发展的因素及对策

目前农村第三产业严重滞后于第一、第二产业,制约了农村经济的发展,主要原因是农村的产业结构不合理,社会服务体系不健全,对农村第三产业重视程度不够等,因此应进一步完善农村服务化体系,调整农村产业结构,大力发展农村经济。     

Antiferromagnetic-vortex dynamics driven by spin-polarized current in small thin disks

We investigate vortex configuration confined in antiferromagnetic thin disks. By virtue of sublattice mismatch at the disk borders, we propose a model that takes such a magnetostatic-like cost into account. The model predicts that onion-like configuration interpolates between curly and divergent vortex. Concerning its dynamics, it is shown that the vortex acquires oscillatory dynamics with well-defined amplitude and frequency that may be controlled on demand by an alternating spin-polarized current. These findings may be useful for the emerging field of antiferromagnetic topological spintronics, once vortex dynamics may be controlled by purely electronic means.     

A general modal frequency-domain vortex lattice method for aeroelastic analyses

The generalized aerodynamic force (GAF) matrix is derived for the Unsteady Vortex Lattice Method (UVLM) without the assumption of out-of-plane dynamics. As a result, the approach naturally includes in-plane motion and forces unlike the doublet lattice method (DLM). The derived UVLM GAF is therefore applicable to industry-standard techniques for aeroelastic stability analyses, such as the p–k method. In this work, the fluid–structure interpolation is performed with radial basis functions for surface interpolation. The generalized aerodynamic forces computed with the UVLM are verified against the DLM from NASTRAN on a simple flat plate configuration. The ability of the UVLM to include steady loads is verified with a T-tail flutter case and the results confirm the importance of including steady loads for T-tail flutter analysis. The modal frequency domain VLM therefore provides the same level of efficiency and accuracy than the DLM, but without the restrictions and with the ability to handle complex geometries. It is therefore a viable replacement to the DLM.