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涡旋射流控制扩压器分离流动的大涡模拟 被引量:7
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作者 樊涛 谢永慧 张荻 《中国电机工程学报》 EI CSCD 北大核心 2008年第35期57-65,共9页
为研究涡旋射流对湍流边界层分离控制的机理,基于大涡模拟方法建立了具有涡旋射流、扩张角为14°的圆锥扩压器数值分析模型,计算结果与相应试验数据吻合良好,验证了计算模型的合理性与精确性。通过对特征截面上流场参数的详细分析,... 为研究涡旋射流对湍流边界层分离控制的机理,基于大涡模拟方法建立了具有涡旋射流、扩张角为14°的圆锥扩压器数值分析模型,计算结果与相应试验数据吻合良好,验证了计算模型的合理性与精确性。通过对特征截面上流场参数的详细分析,获得了射流导致的复杂涡系形成过程,发现了射流孔附近的强涡来源于剪切层涡,剪切层涡经过破碎和耗散,在射流下游近区发展为强弱不对称的反向涡对,在下游远区形成一个纵向涡旋,该涡旋将主流流场边界层外的高能流体卷入到边界层内,增加了边界层内部的流动能量,从而延缓或抑制了流动分离。与相同条件下未采用涡旋射流控制的扩压器相比,其压力恢复系数增加19.8%,表明涡旋射流是一种有效的边界层分离控制方法。文中还分析了不同射流孔数和射流倾斜角对于压力恢复系数的影响,发现选择合适的涡旋射流孔数及其射流倾斜角等参数,可以更有效的控制扩压器内流动分离。 展开更多
关键词 流动控制 涡旋射流 流动分离 大涡模拟
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涡旋射流控制逆压梯度平板边界层分离的涡结构研究 被引量:4
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作者 张荻 樊涛 +1 位作者 蓝吉兵 谢永慧 《西安交通大学学报》 EI CAS CSCD 北大核心 2012年第1期1-8,共8页
为了研究涡旋射流控制边界层分离的物理机理,设计、搭建了涡旋射流控制逆压梯度平板边界层分离实验台,在此基础上对低雷诺数下平板边界层分离及射流控制进行了实验和数值研究.通过对比不同射流控制方式的统计特性及射流控制效果,揭示了... 为了研究涡旋射流控制边界层分离的物理机理,设计、搭建了涡旋射流控制逆压梯度平板边界层分离实验台,在此基础上对低雷诺数下平板边界层分离及射流控制进行了实验和数值研究.通过对比不同射流控制方式的统计特性及射流控制效果,揭示了射流流场大尺度相干结构的演化规律.射流瞬时流动细节的研究表明:发卡涡和类发卡涡是逆压梯度环境下直射流和斜射流中比较典型的涡结构;在斜射流中,随着类发卡涡的发展,射流孔下游发展成熟的类发卡涡涡腿外侧出现了不断增强的次生流向涡结构;次生涡结构对壁面附近能量的增大和质量的输运、耗散具有重要的作用.经对比发现,斜射流控制流动分离的效果明显优于直射流. 展开更多
关键词 流动控制 涡旋射流 大涡模拟 粒子成像测速
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定常与脉冲涡旋射流下矩形扩压器流动分离控制研究
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作者 谢永慧 樊涛 张荻 《西安交通大学学报》 EI CAS CSCD 北大核心 2010年第11期1-5,22,共6页
为了研究涡旋射流控制流动分离的物理机理,基于大涡模拟方法对涡旋射流控制下的矩形扩压器流场和射流流向涡结构的生成、发展等动力学演化过程进行了数值研究.结果表明:射流产生的流向涡将主流高动量气流带入分离区,增加了边界层内气流... 为了研究涡旋射流控制流动分离的物理机理,基于大涡模拟方法对涡旋射流控制下的矩形扩压器流场和射流流向涡结构的生成、发展等动力学演化过程进行了数值研究.结果表明:射流产生的流向涡将主流高动量气流带入分离区,增加了边界层内气流流动方向的动量,使流动分离得到了抑制.射流流场的涡结构主要由射流剪切层涡、马蹄涡、尾涡组成,由于速度梯度大小的变化,使得射流剪切层涡系的结构随着时间推移从涡卷演化为涡环.对于脉冲射流,在低频脉冲下,射流产生的流向涡呈涡卷结构,流动控制效果明显.在高频脉冲下,射流剪切层涡演变成间歇涡环结构,流动控制效果减弱.通过对比脉冲频率和占空比对流动控制的影响发现,占空比为0.5、频率为20Hz的脉冲射流具有较好的流动控制效果. 展开更多
关键词 流动分离 流动控制 涡旋射流 大涡模拟 涡结构
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利用涡流空化效应降解水中罗丹明B 被引量:11
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作者 王金刚 王西奎 +3 位作者 郭培全 国伟林 李桂芳 陆道刚 《中国环境科学》 EI CAS CSCD 北大核心 2007年第1期129-131,共3页
涡流空化通过特殊结构的涡流仓产生,流体在涡流仓中形成压力远低于大气压力的低压区域,从而产生空化效应.通过CFX计算软件对涡流形成情况进行了模拟计算,确定了适宜的结构参数.对罗丹明B进行了实际降解试验,考察了压力和温度对降解的影... 涡流空化通过特殊结构的涡流仓产生,流体在涡流仓中形成压力远低于大气压力的低压区域,从而产生空化效应.通过CFX计算软件对涡流形成情况进行了模拟计算,确定了适宜的结构参数.对罗丹明B进行了实际降解试验,考察了压力和温度对降解的影响,结果表明,压力提高对降解有利,而温度的影响有一定复杂性.涡流空化降解和超声空化降解的对比试验结果表明,涡流空化降解效率远大于超声空化. 展开更多
关键词 空化效应 涡旋射流 罗丹明B 降解
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矩形扩压通道内流动控制的实验与数值研究 被引量:2
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作者 谢永慧 樊涛 +2 位作者 张荻 叶冬挺 王顺森 《中国电机工程学报》 EI CSCD 北大核心 2010年第5期92-99,共8页
采用粒子成像测速技术和大涡模拟方法对带有涡旋射流的矩形扩压器分离控制的流场进行了实验和数值分析,数值计算结果与实验数据吻合良好。通过分析实验和计算得到相关截面速度和涡量分布,讨论了涡旋射流的二维涡结构;同时应用三维涡识... 采用粒子成像测速技术和大涡模拟方法对带有涡旋射流的矩形扩压器分离控制的流场进行了实验和数值分析,数值计算结果与实验数据吻合良好。通过分析实验和计算得到相关截面速度和涡量分布,讨论了涡旋射流的二维涡结构;同时应用三维涡识别技术获得了射流产生各种涡旋结构的流动形态,重点研究射流流向涡结构的生成、发展等动力学演化过程。结果表明:射流剪切层涡系的结构随着时间推移从涡卷演化为了涡环;射流孔口前缘的马蹄涡系具有较强的稳定性,反向涡对具有明显的时均特性。此外还通过对比射流控制前后扩压器表面压力系数、分离区长度、扩张段流动形态及观测点功率谱分析等多种方式探讨了射流控制流动分离的控制效果,并指出射流在下游远场形成的纵向涡旋将主流流场边界层外的高能流体卷入到边界层内,增加了边界层内部的流动能量,从而延缓或抑制了流动分离。 展开更多
关键词 流动控制 涡旋射流 粒子成像测速 大涡模拟
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Swirl Jets in Crossflow at Low Velocity Ratios
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作者 Alexandros Terzis Charilaos Kazakos +2 位作者 Anestis I. Kalfas PavIos K. Zachos Peter Ott 《Journal of Mechanics Engineering and Automation》 2012年第4期256-266,共11页
This investigation examines experimentally the behavior of swirled jets produced by axial flow fans blowing into a crossflow at low velocity ratios. The main difference with non-swirl cases is an asymmetry of the domi... This investigation examines experimentally the behavior of swirled jets produced by axial flow fans blowing into a crossflow at low velocity ratios. The main difference with non-swirl cases is an asymmetry of the dominant kidney vortex and a slight distortion of the jet trace downstream of the injection hole. The effect of jet rotation at relatively low swirl numbers and similar velocity ratios is also investigated by a validated computational analysis tool. The numerical results are analyzed by means of various post-processing procedures, aiming to clarify, quantify and analyze the impact of swirl on the characteristics and the flow domain of a jet in crossflow. In general, swirl introduces an asymmetry in all examined quantities and prevents the penetration of the jet into the crossflow, causing the jet to remain closer to the wall surface. The rotation of the injected fluid results in an imparity of the two parts of the Counter Rotating Vortex Pair (CVP) which is no longer symmetric to the axial centerline plane. High swirl numbers result in the destruction of the CVP and the dominant kidney shape vortex is transformed into a comma shape vortex, rotating close to the wall. 展开更多
关键词 Jet in crossflow SWIRL CFD (computational fluid dynamics).
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Laws of Jet Mixing of the Swirled Flows in a Pipe
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作者 Nikolay Shishkin 《Journal of Energy and Power Engineering》 2013年第7期1223-1230,共8页
Results of experimental research of the mixing process of coaxial flows in a pipe with swirled peripheral jet are presented in this paper. Distribution of temperature and concentration of gases on the axis and wall of... Results of experimental research of the mixing process of coaxial flows in a pipe with swirled peripheral jet are presented in this paper. Distribution of temperature and concentration of gases on the axis and wall of the channel under the influence of such factors as the regime flow, ratio of density of flows and swirl degree of the peripheral jet are studied. Research of temperature, swirl angle, circulation in cross sections along with the channel have shown that their distributions have the jet-like character and are described by known dependences for the layer of mixture. 展开更多
关键词 Film cooling adiabatic jet mixing swirl flow.
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Characteristics of annular impinging jets with/without swirling flow by short guide vanes 被引量:6
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作者 YANG HuiQun KIM TongBeum LU TianJian 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第3期749-757,共9页
Annular jets impinging on a uniformly heated flat plate with or without swirling flow by short guide vanes are experimentally characterized. With the Reynolds number fixed at a relatively low value, the variation of j... Annular jets impinging on a uniformly heated flat plate with or without swirling flow by short guide vanes are experimentally characterized. With the Reynolds number fixed at a relatively low value, the variation of jet flow structures with impinging distance is characterized using the technique of particle image velocimetry (PIV). Correspondingly, the distributions of wall pressure and heat transfer on the plate are measured. At sufficiently large impinging distances, without swirling flow, the obtained flow and wall pressure/heat transfer data are consistent with the classical observation for a conventional annular impinging jet, showing the transition from annular impinging jet flow to single circular impinging jet-like flow. In contrast, no such transition occurs in the presence of flow turning by short guide vanes. At short and intermediate impinging distances, flow turning causes more non-uniform distributions of wall pressure and heat transfer on the target plate and the local heat transfer rates higher than those of the conventional annular jet. This is attributed to the vortical flow structures shed and convected downstream from the short guide vanes. In sharp contrast, at large impinging distances, the larger momentum loss due to flow turning results in lower heat transfer rates on the plate. 展开更多
关键词 annular impinging jet flow structure swirling flow guide vanes wall heat transfer wall pressure
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Large Eddy Simulation of Swirling Jet in a Bluff-Body Burner
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作者 Yohei FUJIMOTO Yuzo INOKUCHI Nobuhiko YAMASAKI 《Journal of Thermal Science》 SCIE EI CAS CSCD 2005年第1期28-33,共6页
The large eddy simulation (LES) is applied to an unconfined swirling flow of an air surrounding a bluff-body having a central jet of air, and the complicated flowfield that involves the recirculation and vortex breakd... The large eddy simulation (LES) is applied to an unconfined swirling flow of an air surrounding a bluff-body having a central jet of air, and the complicated flowfield that involves the recirculation and vortex breakdown is investigated. The Smagorinsky model is used as the sub-grid scale model. The results of the present numerical simulation are compared with the experimental data of the mean and stochastic root mean square (RMS) variations of two velocity components. Although the inflow conditions are specified in a simple manner, the obtained numerical results are in reasonable agreement with the experiments, except for a part of RMS variation values near downstream of the bluff body. The present numerical calculations can successfully reproduce the two characteristics of the flow, i.e., an upstream recirculation zone established just downstream of the burner plane and the additional recirculation zone established at the more downstream location. 展开更多
关键词 large eddy simulation SWIRL BLUFF-BODY recirculation.
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Large Eddy Simulation of Coherent Structure of Impinging Jet
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作者 MingzhouYU LihuaCHEN HanhuiJIN JianrenFAN 《Journal of Thermal Science》 SCIE EI CAS CSCD 2005年第2期150-155,共6页
The flow field of a rectangular exit, semi-confined and submerged turbulent jet impinging orthogonally on a flat plate with Reynolds number 8500 was studied by large eddy simulation (LES). A dynamic sub-grid stress mo... The flow field of a rectangular exit, semi-confined and submerged turbulent jet impinging orthogonally on a flat plate with Reynolds number 8500 was studied by large eddy simulation (LES). A dynamic sub-grid stress model has been used for the small scales of turbulence. The evolvements such as the forming, developing, moving,pairing and merging of the coherent structures of vortex in the whole regions were obtained. The results revealed that the primary vortex structures were generated periodically, which was the key factor to make the secondary vortices generate in the wall jet region. In addition, the eddy intensity of the primary vortices and the secondary vortices induced by the primary vortices along with the time were also analyzed. 展开更多
关键词 large eddy simulation impinging jet coherent structure.
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