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高速压气机叶栅旋涡结构及其流动损失研究 被引量:20
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作者 张海灯 吴云 +1 位作者 李应红 赵勤 《航空学报》 EI CAS CSCD 北大核心 2014年第9期2438-2450,共13页
为揭示高亚声速来流条件下压气机叶栅内部流动特性,对高速压气机叶栅通道内旋涡结构和流动损失的产生与演变规律进行研究。首先建立了数值仿真模型并用实验验证,然后详细研究了叶栅通道内主要旋涡结构、拓扑规律和旋涡模型,最后分析了... 为揭示高亚声速来流条件下压气机叶栅内部流动特性,对高速压气机叶栅通道内旋涡结构和流动损失的产生与演变规律进行研究。首先建立了数值仿真模型并用实验验证,然后详细研究了叶栅通道内主要旋涡结构、拓扑规律和旋涡模型,最后分析了叶栅通道内流动损失与旋涡结构的内在联系。高速压气机叶栅通道内主要存在马蹄涡、端壁展向涡、通道涡、壁角涡、壁面涡、集中脱落涡和尾缘脱落涡7个集中涡系,通道涡由端壁来流附面层中发展而来,是角区复杂旋涡结构的主要诱因;攻角由0°增大为4°,通道涡的涡核更早地脱落端壁附面层向角区发展,但对角区流动的影响减弱,叶片尾缘未形成明显的集中脱落涡。伴随着集中脱落涡的消失,叶栅固壁面拓扑结构中,叶片尾缘吸力面上没有出现与集中脱落涡对应的分离螺旋点,并且与叶中脱落涡层相对应的分离线和再附线消失,尾缘脱落涡仅包含近端区的一个分支。由总压损失沿流向和展向的变化规律,叶栅通道流动损失主要来源于角区复杂旋涡结构引起的强剪切作用,近端壁区的总压损失与角区主要涡系结构的生成和发展密切相关;攻角由0°增大至4°,角区旋涡的影响能力变弱,近端区流动损失减小,与叶中部位总压损失的差异缩小。 展开更多
关键词 高速压气机叶栅 轴向涡量 拓扑规律 旋涡结构 流动损失
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具有叶顶间隙的涡轮正弯叶栅流场的拓扑与旋涡结构 被引量:10
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作者 韩万今 钟兢军 +1 位作者 黄洪雁 王仲奇 《空气动力学学报》 CSCD 北大核心 1999年第2期141-149,共9页
为进一步揭示在具有间隙的涡轮叶栅中叶片正弯降低泄漏损失的机理,采用微型束状与球头五孔测针详细测量了直叶栅和正弯叶栅间隙内和诸横截面流场中的气动参数,并对壁面(包括上、下端壁和叶片表面)进行了墨迹显示。根据测量与显示结... 为进一步揭示在具有间隙的涡轮叶栅中叶片正弯降低泄漏损失的机理,采用微型束状与球头五孔测针详细测量了直叶栅和正弯叶栅间隙内和诸横截面流场中的气动参数,并对壁面(包括上、下端壁和叶片表面)进行了墨迹显示。根据测量与显示结果,应用拓扑学原理分析了壁面与横截面流动的拓扑结构,推测出叶栅内流场的旋涡结构。分析结果表明,在直叶栅中存在着七条分离线与七大集中涡系,它们分别为上端壁叶顶进口吸力边与压力边马蹄涡、泄漏涡、二次涡、下端壁进口边马蹄涡和上、下通道涡。与直叶栅比较,叶片正弯明显减少了壁面与横截面流场中奇点的数量,消除了上通道涡,并使叶顶吸力边的二次涡分离流动由闭式分离转变为开式分离。 展开更多
关键词 涡轮 叶栅 叶顶间隙 正弯叶片 拓扑 旋涡结构
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Study on local topology model of low/high streak structures in wall-bounded turbulence by tomographic time-resolved particle image velocimetry 被引量:6
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作者 Haiping TIAN Nan JIANG +1 位作者 Yongxiang HUANG Shaoqiong YANG 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2015年第9期1121-1130,共10页
The relationship between the in the logarithmic law (log-law) region of bursting event and the low/high-speed streak a turbulent boundary layer is investigated. A tomographic time-resolved particle image velocimetry... The relationship between the in the logarithmic law (log-law) region of bursting event and the low/high-speed streak a turbulent boundary layer is investigated. A tomographic time-resolved particle image velocimetry (TRPIV) system is used to measure the instantaneous three-dimensional-three-component (3D-3C) velocity field. The momentum thickness based Reynolds number is about 2 460. The topological information in the log-law region is obtained experimentally. It is found that the existence of the quadrupole topological structure implies a three-pair hairpin-like vortex packet, which is in connection with the low/high-speed streak. An idealized 3D topological model is then proposed to characterize the observed hairpin vortex packet and low/high-speed streak. 展开更多
关键词 wall turbulence quadrupole topological structure hairpin vortex low/highspeed streak tomographic time-resolved particle image velocimetry (TRPIV) system
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Investigation of the Vortex Dynamic Mechanism of the Flow Losses on a Transonic Compressor Stator 被引量:3
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作者 KAN Xiaoxu WANG Songtao +1 位作者 LUO Lei SU Jiexian 《Journal of Thermal Science》 SCIE EI CAS CSCD 2019年第1期51-60,共10页
For a transonic axial-flow compressor, the numerical simulations, verified against experimental data, were used to study the inherent correlation between the evolutionary process of the vortex structures and the flow ... For a transonic axial-flow compressor, the numerical simulations, verified against experimental data, were used to study the inherent correlation between the evolutionary process of the vortex structures and the flow loss in a compressor stator passage during the throttling process. The flow loss was divided accurately and quantitatively, based on the evolutionary process of the vortex structures. According to the position of the singular points of the vortex structures, the influence of the evolution of the vortex structures on the generation and development of the flow loss was analyzed on a microscale scale. Thereafter, this paper provided the vortex dynamic mechanism of the flow loss, which was important to enrich the theoretical system of the flow field in the compressor. The results show that: the flow loss at the top of the stator tip is caused by the low-energy fluid clusters, which are transported and accumulated by the vortices from the endwall; the transport effect of the pressure separation vortex at the upper half-height only migrates the position of the flow losses, but there is new flow loss generated by its shear action to the endwall. The dominant flow loss during the throttling process concentrates upon the closed separation bubble around the middle of the suction side of the stator. 展开更多
关键词 TRANSONIC COMPRESSOR STATOR throttling process vortex structure flow LOSSES topological analysis
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TOPOLOGICAL STRUCTURES OF VORTEX AND HELICITY ANALYSIS 被引量:1
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作者 黄永念 苏卫东 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1998年第3期208-214,共7页
The topological structures of the vortex filaments and vortex tubes with an exact solution of a straight spiral vortex tube are discussed. It is found that there are some confusions about the calculation of the helic... The topological structures of the vortex filaments and vortex tubes with an exact solution of a straight spiral vortex tube are discussed. It is found that there are some confusions about the calculation of the helicity of a knotted vortex filament and some linked vortex filaments by using different methods. How to unify these methods is explained and the right results are given. (Edited author abstract) 5 Refs. 展开更多
关键词 topological structure vortex filament HELICITY knot and link
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Topological Structure of Vortex Solution in Jackiw-Pi Model
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作者 LI Xi-Guo LIU Zi-Yu LI Yong-Qing GAO Yuan GUO Yan-Rui XIAO Guo-Qing1 Institute of Modern Physics,the Chinese Academy of Sciences,P.O.Box 31,Lanzhou 730000,China2 Graduate School,the Chinese Academy of Sciences,Beijing 100049,China3 Center of Theoretical Nuclear Physics,National Laboratory of Heavy Ion Collisions,Lanzhou 730000,China 《Communications in Theoretical Physics》 SCIE CAS CSCD 2007年第7期143-146,共4页
By using φ-mapping method,we discuss the topological structure of the self-duality solution in Jackiw-Pimodel in terms of gauge potential decomposition.We set up relationship between Chern-Simons vortex solution andt... By using φ-mapping method,we discuss the topological structure of the self-duality solution in Jackiw-Pimodel in terms of gauge potential decomposition.We set up relationship between Chern-Simons vortex solution andtopological number,which is determined by Hopf index and Brouwer degree.We also give the quantization of flux inthis ease.Then,we study the angular momentum of the vortex,which can be expressed in terms of,the flux. 展开更多
关键词 topological structure vortex Jackiw-Pi model
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端壁VGJs对高亚音扩压叶栅内分离结构的影响
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作者 陈聪 刘华坪 陈浮 《哈尔滨工程大学学报》 EI CAS CSCD 北大核心 2018年第8期1314-1320,共7页
为揭示栅内射流旋涡发生器(vortex generator jets,VGJs)控制前后叶栅内部流动特性,本文根据拓扑学原理,对某高亚音压气机叶栅通道控制前后分离形态的变化进行了研究,并给出了其拓扑结构及旋涡结构模型,同时对控制前后损失特性变化进行... 为揭示栅内射流旋涡发生器(vortex generator jets,VGJs)控制前后叶栅内部流动特性,本文根据拓扑学原理,对某高亚音压气机叶栅通道控制前后分离形态的变化进行了研究,并给出了其拓扑结构及旋涡结构模型,同时对控制前后损失特性变化进行了分析。计算结果表明:端壁射流旋涡发生器改变了流场的分离结构,有效推迟了吸力面侧的分离。加入流动控制后,奇点数目明显减少,端壁附面层横向迁移被有效抑制,通道涡、集中脱落涡被明显削弱,叶展中部的尾缘脱落涡基本消失,端壁损失以及叶型损失变化不大,二次流动损失明显降低,降低了38%。端壁射流旋涡发生器对叶栅中部影响较弱,因此,有必要采取端壁/吸力面组合流动控制进一步改善流场结构。 展开更多
关键词 扩压叶栅 射流旋涡 拓扑结构 旋涡结构 高亚音 流动分离 射流旋涡发生器
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具有后部加载叶型的环形静叶栅的旋涡结构
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作者 周逊 韩万金 周广勤 《汽轮机技术》 北大核心 2003年第1期34-35,共2页
为了详细研究具有后部加载叶型的环形静叶栅的流场结构,在环形叶栅低速风洞上对具有后部加载叶型的环形弯曲叶片静叶栅上、下端壁以及叶片型面进行了墨迹显示实验,同时应用拓扑学原理分析了叶栅的壁面流谱,并据此分析提出了本实验叶栅... 为了详细研究具有后部加载叶型的环形静叶栅的流场结构,在环形叶栅低速风洞上对具有后部加载叶型的环形弯曲叶片静叶栅上、下端壁以及叶片型面进行了墨迹显示实验,同时应用拓扑学原理分析了叶栅的壁面流谱,并据此分析提出了本实验叶栅的二次流动的拓扑示意图。 展开更多
关键词 环形静叶栅 旋涡结构 流动显示 拓扑原理 汽轮机
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有叶顶间隙的涡轮弯叶栅拓扑与旋涡结构(Ⅱ)——横截面流场拓扑结构与叶栅旋涡结构 被引量:2
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作者 杨庆海 黄洪雁 韩万今 《应用数学和力学》 CSCD 北大核心 2002年第8期851-854,共4页
根据具有叶顶间隙的直叶栅和正、反弯叶栅壁面流动的墨迹显示以及横截面内气动参数测量 ,应用拓扑学原理 ,分析了叶栅流道横截面内的拓扑结构· 与直叶栅比较 ,叶片正弯消除了上通道涡分离线 ,并使二次涡由闭式分离转变为开式分离 ... 根据具有叶顶间隙的直叶栅和正、反弯叶栅壁面流动的墨迹显示以及横截面内气动参数测量 ,应用拓扑学原理 ,分析了叶栅流道横截面内的拓扑结构· 与直叶栅比较 ,叶片正弯消除了上通道涡分离线 ,并使二次涡由闭式分离转变为开式分离 ,而叶片反弯仅影响奇点位置、旋涡强度与尺度· 展开更多
关键词 涡轮叶栅 叶顶间隙 弯叶栅 端壁 叶片表面 拓扑结构
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TOPOLOGY AND VORTEX STRUCTURES OF A CURVING TURBINE CASCADE WITH TIP CLEARANCE (Ⅱ)- TOPOLOGICAL FLOW PATTERN AND VORTEX STRUCTURE IN THE TRANSVERSE SECTION OF A BLADE CASCADE
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作者 杨庆海 黄洪雁 韩万今 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2002年第8期958-962,共5页
By means of ink trace visualization of the flows in conventional straight, positively curved and negatively curved cascades with tip clearance, and measurement of the aerodynamic parameters in transverse section, and... By means of ink trace visualization of the flows in conventional straight, positively curved and negatively curved cascades with tip clearance, and measurement of the aerodynamic parameters in transverse section, and by appling topology theory, the topological structures and vortex structure in the transverse section of a blade cascade were analyzed. Compared with conventional straight cascade, blade positive curving eliminates the separation line of the upper passage vortex, and leads the secondary vortex to change from close separation to open separation, while blade negative curving effects merely the positions of singular points and the intensities and scales of vortex. 展开更多
关键词 turbine cascade tip clearance curving cascade transverse section flow field topological flow pattern and vortex structure
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