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3D LDV MEASUREMENTS OF ROTOR BLADE TIP VORTEX IN HOVER
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作者 李峰 康浩 高正 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 1996年第2期11+7-10,共5页
An investigation made on the rotor blade tip vortex through use of a Three Dimensional Laser Doppler Velocimetry(3D LDV) is described. The experiment is conducted with a 2 m in diameter model helicopter rotor. By a ... An investigation made on the rotor blade tip vortex through use of a Three Dimensional Laser Doppler Velocimetry(3D LDV) is described. The experiment is conducted with a 2 m in diameter model helicopter rotor. By a series of measurements near blade tip, the velocity field near blade tip is documented, and through which, the tip vortex rollup and development are presented. The radial distribution of instantaneous velocities at various levels above and under the rotor disc is also measured in this investigation. Using this distribution, the influence of the tip vortex from the preceding blade on the follow up blade is discussed. 展开更多
关键词 rotors flow fields blade tip 3D ldv measurement
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EXPERIMENTAL INVESTIGATION FOR THE EFFECT OF ROTATION ON THREE-DIMENSIONAL FLOW FIELD IN FILM-COOLED TURBINE 被引量:2
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作者 YUAN Feng ZHU Xiaocheng DU Zhaohui 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2007年第1期10-15,共6页
An experimental investigation of three-dimensional flow field in a film-cooled turbine model is carried out by using particle image velocimeter (PIV) in a low-speed wind tunnel. The effects of different blowing rati... An experimental investigation of three-dimensional flow field in a film-cooled turbine model is carried out by using particle image velocimeter (PIV) in a low-speed wind tunnel. The effects of different blowing ratios (M=1.5, 2) on the flow field are studied. The experimental results reveal the classical phenomena of the formation of kidney vortex pair and secondary flow in wake region behind the jet hole. And the changes of the kidney vortex pair and the wake at different locations away from the hole on the suction and pressure sides are also studied. Compared with the flow field in stationary cascade, there are centrifugal force and Coriolis force existing in the flow field of rotating turbine, and these forces bring the radial velocity in the jet flow. The effect of rotatien on the flow field of the pressure side is more distinct than that on the suction side from the measured flow fields in Y-Z plane and radial velocity contours. The increase of blowing ratio makes the kidney vortex pair and the secondary flow in the wake region stronger and makes the range of the wake region enlarged. 展开更多
关键词 Film-cooled turbine rotor PIV measurement Blowing ratio three-dimensional flow field
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AN APPLICATION OF TOPOLOGICAL METHOD TO ANALYSING THE THREE-DIMENSIONAL FLOW IN CASCADES(Ⅱ)-TOPOLOGICAL ANALYSIS ON THE VECTOR FIELD PATTERNS OF SKINFRICTIONS AND SECTION STREAMLINES
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作者 Kang Shun Wang Zhongqi 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 1990年第12期1119-1127,共9页
With an application of topological analysis,in this paper the skin-friction line patterns on compressor and turbine cascade surfaces are depicted and the streamline patterns of the secondary flow fields in the cross-s... With an application of topological analysis,in this paper the skin-friction line patterns on compressor and turbine cascade surfaces are depicted and the streamline patterns of the secondary flow fields in the cross-section of a curved pipe and a turbine cascade are drawn under given conditions.In addition the structures of vortices within three-dimensional viscous flow fields in cascades are analysed. 展开更多
关键词 topological analysis separation flow three-dimensional flow visualization turbine COMPRESSOR vortex
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Grid Convergence Property of Three-Dimensional Measurement-Integrated Simulation for Unsteady Flow behind a Square Cylinder with Karman Vortex Street
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作者 Takayuki Yamagata Toshiyuki Hayase 《Journal of Flow Control, Measurement & Visualization》 2016年第4期125-142,共18页
The purpose of this study was to clarify grid convergence property of three-dimensional measurement-integrated (3D-MI) simulation for a flow behind a square cylinder with Karman vortex street. Measurement-integrated (... The purpose of this study was to clarify grid convergence property of three-dimensional measurement-integrated (3D-MI) simulation for a flow behind a square cylinder with Karman vortex street. Measurement-integrated (MI) simulation is a kind of the observer in the dynamical system theory by using CFD scheme as a mathematical model of the system. In a former study, two-dimensional MI (2D-MI) simulation with a coarse grid system showed a fairly good result in comparison with a 2D ordinary (2D-O) simulation, but the results were degraded with grid refinement. In this study, 3D-MI simulation and three-dimensional ordinary (3D-O) simulation were performed with three grid systems of different grid resolutions, and their grid convergence properties were compared. As a result, all 3D-MI simulations reproduced the vortex shedding frequency identical to that of the experiment, and the flow fields obtained were very close, within 5% difference between the results, while the results of the 3D-O simulations showed variation of the solution under convergence. It is shown that the grid convergence property of 3D-MI simulation is monotonic and better than that of 3D-O simulation, whereas those of 2D-O and 2D-MI simulations for streamwise velocity fluctuation are divergent. The solution of 3D-MI simulation with a relatively coarse grid system properly reproduces the basic three-dimensional structure of the wake flow as well as the drag and lift coefficients. 展开更多
关键词 measurement-Integrated Simulation Grid Convergence Square Cylinder flow measurement Numerical Simulation Pressure measurement flow Observer Karman vortex
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Study on Blade Surface Flow around Wind Turbine by Using LDV Measurements 被引量:4
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作者 Tinnapob Phengpom Yasunari Kamada +3 位作者 Takao Maeda Junsuke Murata Shogo Nishimura Tasuku Matsuno 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第2期131-139,共9页
This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade i... This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade is a challenging endeavor. In this research, the HAWT model with 2.4 m diameter was tested in the large wind tunnel. The flow around the rotating blade surface was measured simultaneously for three velocity components, and two probes were used for the synchronized measurement of three-dimensional flow components. The local velocity was detected for the single seeding particle measured in the point where three pairs of laser beams intersected. Blade sections of interest in this study are composed of radial positions r/R = 0.3, 0.5 and 0.7. Optimum and low tip speed ratio flow characteristics were also compared. The velocity flow vector, skin friction coefficient and bound circulation were calculated from LDV measurements, and the experimental research showed reasonably and clearly the experimental results. 展开更多
关键词 ldv measurement Sectional performance Wind turbine Boundary layer flow Span-wise flow
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A Study on Swirling Flows in a Rectangular Channel(LDV Measurement, Flow Visualization and Large Eddy Simulation) 被引量:1
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作者 Kazuyoshi MATSUZAKI ,Yasutake HARAMOTO ,Mizue MUNEKATA Hideki OHBA Dept. of Mechanical Engineering and Materials Science, Kumamoto University, Kurokami 2-39-1,Kumamoto, 860-8555, Japan 《Journal of Thermal Science》 SCIE EI CAS CSCD 2001年第3期205-210,共6页
The purpose of this study is to make clear the behavior of swirling pipe flows with non-circular section. We have investigated experimentally and numerically the swirling flows in a rectangular channel with aspect rat... The purpose of this study is to make clear the behavior of swirling pipe flows with non-circular section. We have investigated experimentally and numerically the swirling flows in a rectangular channel with aspect ratio of 1.3, which is one of the typical pipe flow with non-circular section. In this paper, experimental apparatus with water circulation system is produced, and LDV measurement of the swirling flows is performed in order to clarify the mean velocities and turbulent quantity with higher accuracy. In addition, flow visualization for movement of vortex core region in the swirling flows is carried out using tracer method. Moreover, large eddy simulation (LES) of the flow field is made and compared with the experimental results. As results of these investigations, the behavior of the swirling flows in the rectangular channel is totally discussed. 展开更多
关键词 swirling flow ldv measurement flow visualization large eddy simulation.
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基于2D-LDV技术的船舶螺旋桨三维流场结构分析(英文) 被引量:5
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作者 李广年 吴卫国 +3 位作者 张军 谢永和 胡小菲 白兴兰 《空气动力学学报》 CSCD 北大核心 2014年第5期700-704,共5页
利用2D-LDV设备,通过优化布置测试点,获得了均匀来流下螺旋桨尾流场三维流动数据。展示了宏观的流场动态以及微观的流动信息,如尾涡和梢涡在流场中的分布情况、尾涡部流动的剪切效应、梢涡部的绕流及流动分离状态。计算了水动力螺距角... 利用2D-LDV设备,通过优化布置测试点,获得了均匀来流下螺旋桨尾流场三维流动数据。展示了宏观的流场动态以及微观的流动信息,如尾涡和梢涡在流场中的分布情况、尾涡部流动的剪切效应、梢涡部的绕流及流动分离状态。计算了水动力螺距角以及螺旋桨附着涡的总环量。试验显示了LDV技术在流动细节测试方面的优势,获得的定量信息可以为相关研究人员提供技术支持。 展开更多
关键词 螺旋桨尾流 流动分离 水动力螺距角 环量 ldv
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离心泵蜗壳内部高粘油时均流动的LDV测量 被引量:3
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作者 李文广 薛敦松 朱宏武 《工程热物理学报》 EI CAS CSCD 北大核心 1997年第1期61-64,共4页
本文用LDV测量了最优工况和小流量工况下,输送运动粘度为48mm2/s高粘油时,蜗壳第Ⅳ、Ⅵ和Ⅷ断面内的时均切向、径向速度。给出了角动量随半径的变化关系,并与输送粘度为1mm2/s水时的角动量进行了比较。
关键词 离心泵 蜗壳 高粘油 流动测量 ldv
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周期性瞬态喷雾中粒子速度的LDV测量研究 被引量:3
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作者 陈白欣 李宏伟 +1 位作者 腾叙充 王荣生 《内燃机工程》 EI CAS CSCD 北大核心 1992年第3期44-50,66,共8页
本文应用非实时测量原理成功地研制了一套适用于周期性瞬态测量的计数式LDV系统。用该系统测量了空气压力为1.0MPa、室温环境下,圆孔式和伞喷式两种喷嘴产生的瞬态喷雾中油粒子的轴向速度分量的时空分布。研究了不同5/8比较精度下,采样... 本文应用非实时测量原理成功地研制了一套适用于周期性瞬态测量的计数式LDV系统。用该系统测量了空气压力为1.0MPa、室温环境下,圆孔式和伞喷式两种喷嘴产生的瞬态喷雾中油粒子的轴向速度分量的时空分布。研究了不同5/8比较精度下,采样次数对测量精度的影响。分析了实验误差。 展开更多
关键词 瞬态喷雾 两相流动 速度场 ldv测量
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基于LDV技术的螺旋桨尾涡测试 被引量:6
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作者 李广年 《实验流体力学》 EI CAS CSCD 北大核心 2010年第4期75-79,共5页
对螺旋桨尾流场LDV(Laser Doppler Velocimeter)测试数据进行了详细的分析,比较了均匀来流下螺旋桨尾流中两个横断面上的流动信息,以及同一横断面上不同半径处轴向、径向速度沿周向的分布,试验数据不仅显示了尾流场宏观流动现象,而且也... 对螺旋桨尾流场LDV(Laser Doppler Velocimeter)测试数据进行了详细的分析,比较了均匀来流下螺旋桨尾流中两个横断面上的流动信息,以及同一横断面上不同半径处轴向、径向速度沿周向的分布,试验数据不仅显示了尾流场宏观流动现象,而且也清晰的显示了诸如在周向仅有8°跨越的速度突变等微观流动信息,数据分析显示试验结果与理论分析比较吻合。试验所获得的定量信息可以为尾流场复杂流动现象的揭示、螺旋桨非定常性能的预报以及螺旋桨设计提供参考。 展开更多
关键词 流体测试 ldv 螺旋桨 尾涡 梢涡
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LDV实验测量气冷环形涡轮叶栅内部流场 被引量:2
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作者 袁锋 吴亚东 +1 位作者 竺晓程 杜朝辉 《热能动力工程》 EI CAS CSCD 北大核心 2007年第6期596-600,共5页
采用LDV对气冷环形涡轮叶栅流场三维平均速度进行实验测量,研究孔射流对环形涡轮叶栅流场的影响。实验结果表明,由于孔射流的影响,在孔下游靠近叶片表面处形成回流区,回流区速度随着下游距离的增加逐渐减弱,同时射流在与主流的掺混过程... 采用LDV对气冷环形涡轮叶栅流场三维平均速度进行实验测量,研究孔射流对环形涡轮叶栅流场的影响。实验结果表明,由于孔射流的影响,在孔下游靠近叶片表面处形成回流区,回流区速度随着下游距离的增加逐渐减弱,同时射流在与主流的掺混过程中产生反向涡对。在涡轮叶片的吸力面和压力面,由于壁面曲率、来流附面层状态和压力梯度的差异,射流与主流的掺混以及流场结构也有所不同。在压力面侧,射流与主流掺混形成的反向涡对比较明显,射流尾迹的影响范围也较吸力面大。 展开更多
关键词 ldv测量 环形涡轮叶栅 孔射流 三维平均速度
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涡轮级轮缘封严内非定常流场的准三维LDV测量 被引量:14
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作者 马宏伟 Dieter E Bohn +1 位作者 Achim Decker Bernd Rudzinski 《航空动力学报》 EI CAS CSCD 北大核心 2004年第4期455-458,共4页
研究涡轮级封严内流动和主流的相互作用、相互影响,进一步认识盘腔内燃气入侵等非定常现象,急需流场实验数据验证。针对轮缘封严内空间狭窄、光路安排困难等问题,本文发展了一种用于测量涡轮级轮缘封严内非定常流场的准三维LDV技术,即... 研究涡轮级封严内流动和主流的相互作用、相互影响,进一步认识盘腔内燃气入侵等非定常现象,急需流场实验数据验证。针对轮缘封严内空间狭窄、光路安排困难等问题,本文发展了一种用于测量涡轮级轮缘封严内非定常流场的准三维LDV技术,即测量分两步,首先在机匣上安置二维测速系统用符合方式测出径向、切向速度及湍流度,再在轮毂内安置一维探头重复测量,从两次测量数据中计算出轴向速度;该技术借助锁相采样等技术能测出不同动静叶相对位置情况下封严及盘腔内的周期性非定常流场细节,本文给出了部分典型的动态流场测量结果。 展开更多
关键词 航空、航天推进系统 涡轮 轮缘封严 非定常流场 准三维ldv测量
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气固两相流动的LDV测试技术研究与实施 被引量:2
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作者 李玲 李景银 徐忠 《化工机械》 CAS 1998年第6期1-5,15,共6页
介绍了气固两相流动的LDV测试方法和有关技术。并对方管内网栅后气固两相流动进行了测量,固相颗粒平均粒径Dp=900μm,颗粒质量分数α=0.205%、0.30%。试验给出了管内不同断面上气流及颗粒速度分布情况,通过与... 介绍了气固两相流动的LDV测试方法和有关技术。并对方管内网栅后气固两相流动进行了测量,固相颗粒平均粒径Dp=900μm,颗粒质量分数α=0.205%、0.30%。试验给出了管内不同断面上气流及颗粒速度分布情况,通过与纯气流条件下的试验结果比较,分析了不同质量分数的颗粒对气流速度结构的影响,并对同样条件下的颗粒与气流速度分布进行了比较。 展开更多
关键词 气固两相流动 ldv 测量技术 两相流 悬浮流
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方管内气固两相流动速度的LDV测量 被引量:2
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作者 李玲 徐忠 《实验力学》 CSCD 北大核心 1998年第2期267-272,共6页
介绍了气固两相流动的LDV测试方法和有关技术,并给出了方管内网栅后气固两相流动的部分测试结果与分析。对于气相,给出了纯净气流(α=0)、平均粒径dp=350μm的颗粒(α=0.12%、0.21%、0.335%)存在时... 介绍了气固两相流动的LDV测试方法和有关技术,并给出了方管内网栅后气固两相流动的部分测试结果与分析。对于气相,给出了纯净气流(α=0)、平均粒径dp=350μm的颗粒(α=0.12%、0.21%、0.335%)存在时的气流在管内不同断面上时均速度分布情况及不同颗粒浓度时气流速度结构的比较;对于固相,给出了三种不同固相浓度时颗粒在管内不同断面上时均速度的分布情况,并对三种固相浓度时颗粒与气相的速度分布进行了比较。 展开更多
关键词 气固两相流动 时均速度 颗粒浓度 ldv测量
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网栅后湍流流动的LDV测量
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作者 李玲 张义云 徐忠 《水动力学研究与进展(A辑)》 CSCD 北大核心 1998年第1期71-78,共8页
本文应用LDV技术对方管内网栅所形成的湍流流动做了详细测量,获得了管内不同位置湍流流动沿流动方向的衰减规律及网栅后不同距离处方管各断面上的速度及脉动速度分布情况.
关键词 湍流 ldv测量 方管 网栅 速度 脉动速度
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液力变矩器内流场LDV测试散射粒子的选取 被引量:3
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作者 祝自来 李宏才 +1 位作者 闫清东 陈杰翔 《实验技术与管理》 CAS 北大核心 2013年第12期54-57,共4页
基于激光多普勒测速技术(LDV)的基本原理,建立液力变矩器内部流场三维LDV测试系统。从湍流理论出发,通过求解BBO方程,对液力变矩器流道内散射粒子的跟随性进行了计算,详细分析了液力变矩器油液中散射粒子密度和直径对跟随性的影响。研... 基于激光多普勒测速技术(LDV)的基本原理,建立液力变矩器内部流场三维LDV测试系统。从湍流理论出发,通过求解BBO方程,对液力变矩器流道内散射粒子的跟随性进行了计算,详细分析了液力变矩器油液中散射粒子密度和直径对跟随性的影响。研究表明,液力变矩器油液中粒子的跟随性较好,因此选取时主要考虑粒子的散光特性,适当增加粒子的直径,以获得较好的测试信号。 展开更多
关键词 液力变矩器 散射粒子 ldv 流场测试
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涡流管流动结构及能量分离性能LDV实验研究 被引量:2
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作者 郭向吉 胡素锋 +2 位作者 张博 刘博 付庭煌 《大连理工大学学报》 EI CAS CSCD 北大核心 2019年第5期480-491,共12页
设计了直径为30 mm的可组装式透明涡流管以实现主流道可视化,并采用二维激光多普勒测速(LDV)技术得到子午面时均流场.研究了不同冷流比(0.1~0.9)、主流道长度(360、600、900和1 200 mm)、入口压力(0.01、0.02 MPa)下的轴向速度和径向速... 设计了直径为30 mm的可组装式透明涡流管以实现主流道可视化,并采用二维激光多普勒测速(LDV)技术得到子午面时均流场.研究了不同冷流比(0.1~0.9)、主流道长度(360、600、900和1 200 mm)、入口压力(0.01、0.02 MPa)下的轴向速度和径向速度分布,特别是折返流边界对能量分离性能的影响.LDV结果表明,时均轴向速度分布具有较好的轴对称性,不同压力下流动结构具有相似性,径向速度远小于轴向速度.增加冷流比会导致折返流边界径向膨胀,揭示了在过短管和过长管中两种能量分离恶化机制--过短管中折返流面过厚,过长管中轴向滞止点向冷端靠拢.该结果验证了以往所提出的优化准则,同时可以说明滞止点并不是涡流管中的一种基本流动结构. 展开更多
关键词 涡流管 激光多普勒测速(ldv) 流动结构 能量分离性能 折返流边界
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用LDV研究柴油机不同燃烧室对缸内湍流场的影响 被引量:6
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作者 沈建平 吴承雄 +1 位作者 朱隆碧 杨玟 《内燃机学报》 EI CAS CSCD 北大核心 1995年第1期19-27,共9页
本文对两种不同形状的燃烧室,采用激光多普勒测速技术(LDV),在一个测量平面内,测量了轴向和切向的瞬时速度随曲轴转角的变化规律,并采用相平均法,计算了两个方向的平均速度和湍流度。根据测量结果,分析了两种燃烧室结构情形... 本文对两种不同形状的燃烧室,采用激光多普勒测速技术(LDV),在一个测量平面内,测量了轴向和切向的瞬时速度随曲轴转角的变化规律,并采用相平均法,计算了两个方向的平均速度和湍流度。根据测量结果,分析了两种燃烧室结构情形下,气缸内气流运动的规律,并比较了二者的异同,从而阐述了两种燃烧室对油气混合、燃烧、污染物生成影响的不同规律,为燃烧室的合理设计、提高柴油机性能,提供了有力的依据。 展开更多
关键词 燃烧室 流场没量 湍流度 柴油机
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3D FLOW INSIDE BUBBLE-TYPE VORTEX BREAKDOWN: AN EXPERIMENTAL INVESTIGATION VIA LDV 被引量:4
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作者 LiuYing-zheng ChenHan-ping KoyamaHideS 《Journal of Hydrodynamics》 SCIE EI CSCD 2003年第3期44-48,共5页
Bubble-type vortex breakdown of the swirling flow inside a closed cylindricalcontainer with a rotating upper endwall was experimentally investigated via LDV. 3D measurement ofthe steady bubble at H/R =1.5 was firstly ... Bubble-type vortex breakdown of the swirling flow inside a closed cylindricalcontainer with a rotating upper endwall was experimentally investigated via LDV. 3D measurement ofthe steady bubble at H/R =1.5 was firstly carried out with very fine grid arrangement. Flow detailsinside the bubble and its Re -dependent structure were made clear. Abrupt waves of the azimuthalvelocity component were always found to be between the bottom stationary endwall and the upstreamstagnation point, which might be the reason of bubble formation. Variation of bubble structure andbubble center with the increasing Re gives the explanation for the disappearance of the breakdownregion. 展开更多
关键词 bubble-type vortex breakdown ldv swirling flow
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用LDV系统测量转盘萃取塔内流场 被引量:2
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作者 许宏庆 费维扬 《实验力学》 CSCD 北大核心 1995年第4期316-322,共7页
本文应用激光多普勒测速仪对二种转盘萃取塔(RDC)模型进行切向速度、轴向速度和湍流度测量。实验结果表明。在RDC是切向速度比较大,因而有较好的搅拌效果,它的内部流场比较均匀稳定,有利于传质,所以RDC是广泛应用于化学... 本文应用激光多普勒测速仪对二种转盘萃取塔(RDC)模型进行切向速度、轴向速度和湍流度测量。实验结果表明。在RDC是切向速度比较大,因而有较好的搅拌效果,它的内部流场比较均匀稳定,有利于传质,所以RDC是广泛应用于化学工业中的一种液-液萃取设备。 展开更多
关键词 激光多谱勒 测速仪 转盘 萃取塔 流场测量
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