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悬臂方向对TLV空化抑制效果的影响及其机理
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作者 程怀玉 季斌 +1 位作者 龙新平 槐文信 《工程力学》 EI CSCD 北大核心 2022年第5期224-232,共9页
该文综合利用实验及数值模拟方法细致研究了悬臂式沟槽叶顶间隙泄漏涡(tip-leakage vortex, TLV)空化抑制器的悬臂凸出方向对抑制TLV空化效果的影响,并对其原因进行了深入讨论。研究表明:相比于原始水翼叶顶处的TLV空化,无论悬臂凸出方... 该文综合利用实验及数值模拟方法细致研究了悬臂式沟槽叶顶间隙泄漏涡(tip-leakage vortex, TLV)空化抑制器的悬臂凸出方向对抑制TLV空化效果的影响,并对其原因进行了深入讨论。研究表明:相比于原始水翼叶顶处的TLV空化,无论悬臂凸出方向指向水翼的吸力面还是压力面,悬臂式沟槽TLV空化抑制器在各个间隙大小下均能产生显著的抑制效果。相对而言,当所采用的悬臂凸出方向为压力面时,该装置对TLV空化的抑制效果更为显著,且可更有效地抑制TLV空化体积脉动。测量结果表明:悬臂凸出方向对水翼升、阻力系数影响均很小。数值结果则进一步表明:当采用悬臂凸出方向为指向压力面时,悬臂式沟槽TLV空化抑制器能更好地抑制流体从压力面流向吸力面,干扰TLV的生长,进而可以更加有效地抑制TLV空化的发展。 展开更多
关键词 空化 水翼 叶顶间隙泄漏涡 流动控制 泄漏流
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不同空化工况的导管桨梢隙涡空化流场数值分析
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作者 徐顺 刘琦 +2 位作者 张益诚 王俊新 熊永亮 《中国舰船研究》 CSCD 北大核心 2023年第3期122-128,共7页
[目的]旨在研究梢隙涡(TLV)空化发展对涡核特性的影响规律。[方法]结合SST k-ω和ZwartGerber-Belamri空化模型,对不同空化工况下的导管桨梢隙涡空化流场开展数值模拟研究,然后在验证数值模拟可靠性的基础上,基于汽相体积分数等值面图和... [目的]旨在研究梢隙涡(TLV)空化发展对涡核特性的影响规律。[方法]结合SST k-ω和ZwartGerber-Belamri空化模型,对不同空化工况下的导管桨梢隙涡空化流场开展数值模拟研究,然后在验证数值模拟可靠性的基础上,基于汽相体积分数等值面图和Q准则,分别对梢隙涡空化发展及涡核特性演变规律展开研究。[结果]结果显示,梢隙涡空化的发展使得稳定的泄漏流空化面积不断扩大,当发展至特定工况时,梢隙涡空化会在泄漏空化的随边处发生旋拧;若空化继续发展,将对导管桨的性能产生显著影响。空化的发展使得梢隙涡逐渐远离叶片吸力面,并使涡心处的流速分布更为复杂,当空化数σ=1.488时,空化的持续发展会显著降低梢隙涡的强度。随着梢隙涡向下游发展,梢隙涡卷吸来自壁面周向涡量的能力不断减弱,并且间隙处的湍动能会随着梢隙涡的发展逐渐输运至涡心处。[结论]研究方法和研究结果可为水力旋转机械的性能预测和梢隙涡空化的控制提供相应的理论指导。 展开更多
关键词 导管螺旋桨 梢隙涡 空化 数值模拟
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周向槽和阶梯槽在提高轴流压气机稳定工作裕度中的综合利用 被引量:3
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作者 卢家玲 楚武利 卢新根 《机械设计与制造》 北大核心 2007年第9期118-120,共3页
在验证了计算模型的可靠性后,针对西北工业大学某轴流压气机转子的失速类型,进行了周向槽机匣、阶梯槽机匣,以及两者组合结构的扩稳效果的数值模拟。结果表明,周向槽结构在叶片通道前端可起到对叶顶泄漏涡的控制作用,而在叶片通道尾端... 在验证了计算模型的可靠性后,针对西北工业大学某轴流压气机转子的失速类型,进行了周向槽机匣、阶梯槽机匣,以及两者组合结构的扩稳效果的数值模拟。结果表明,周向槽结构在叶片通道前端可起到对叶顶泄漏涡的控制作用,而在叶片通道尾端效果不大。阶梯槽结构在叶片通道后端则能利用流向压差起到扩稳作用。采用叶片通道前部为周向槽,尾部为阶梯槽的组合机匣结构能在效率损失较小的情况下,对类似的压气机起到较理想的扩稳效果。 展开更多
关键词 周向槽 阶梯槽 叶顶泄漏涡 尾迹
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四级低速轴流压气机端壁区流动的实验研究 被引量:1
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作者 张晨凯 胡骏 王志强 《中国机械工程》 EI CAS CSCD 北大核心 2014年第13期1705-1711,共7页
在四级低速大尺度轴流压气机试验台上,利用自行设计加工的十孔梳状附面层探针、四孔探针以及埋入高频响Kulite传感器的动态探针,针对端壁区流动展开了详细的流场测量。从附面层探针测量结果中能清晰识别出附面层区和主流区;获得了该压... 在四级低速大尺度轴流压气机试验台上,利用自行设计加工的十孔梳状附面层探针、四孔探针以及埋入高频响Kulite传感器的动态探针,针对端壁区流动展开了详细的流场测量。从附面层探针测量结果中能清晰识别出附面层区和主流区;获得了该压气机进口的附面层位移厚度、动量损失厚度、能量损失厚度及堵塞系数,且实验结果表明,采用平板紊流附面层公式能较好地进行附面层厚度的估算;采用位移机构带动四孔探针测得的第三级压气机转子进出口流场速度结果显示,受轮毂旋转作用,转子后的下端壁区附面层厚度明显要小于上端壁区附面层厚度;动态探针测量结果能较为明显地识别出叶尖泄漏涡的发展轨迹,且随着流量系数的减小,叶片尖部最大负荷点从尾缘向前缘移动,导致叶尖泄漏涡起始点前移。 展开更多
关键词 端壁附面层 叶尖泄漏涡 旋转失速 压气机
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绕水翼间隙涡结构形成机理与间隙几何影响 被引量:3
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作者 张虎 左逢源 +1 位作者 张德胜 施卫东 《浙江大学学报(工学版)》 EI CAS CSCD 北大核心 2020年第12期2344-2355,共12页
为了分析绕水翼间隙涡结构形成机理和探究压力边圆角几何的影响,对绕NACA0009水翼间隙流动进行数值计算.通过流线涡量云图三维可视化分析,得到间隙流动特征及涡结构,对涡强度进行对比.对翼形中截面间隙进出口边速度和间隙区平面流线、... 为了分析绕水翼间隙涡结构形成机理和探究压力边圆角几何的影响,对绕NACA0009水翼间隙流动进行数值计算.通过流线涡量云图三维可视化分析,得到间隙流动特征及涡结构,对涡强度进行对比.对翼形中截面间隙进出口边速度和间隙区平面流线、压力、湍动能进行比较分析.研究发现:直角叶顶水翼泄漏流在间隙进口边有较大的展向速度,在间隙内形成新月形分离区,在逆压梯度作用下形成叶顶分离涡(TSV),涡尺度与展向速度成正相关;叶顶泄漏涡(TLV)形成源于间隙出口边射流与吸力边侧低速流体之间的持续剪切作用,低速流体从剪切层获得持续的能量输运形成稳定的泄漏涡结构;间隙压力边圆角对TSV起抑制作用,降低了间隙区整体涡强度. 展开更多
关键词 水翼 圆角几何 叶顶分离涡(TSV) 叶顶泄漏涡(tlv) 展向速度 涡结构
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A review of cavitation in tip-leakage flow and its control 被引量:15
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作者 Huai-yu Cheng Bin Ji +2 位作者 Xin-ping Long Wen-xin Huai Mohamed Farhat 《Journal of Hydrodynamics》 SCIE EI CSCD 2021年第2期226-242,共17页
The tip-leakage vortex(TLV)cavitation is a challenging issue for a variety of axial hydraulic turbines and pumps from both technical and scientific viewpoints.The flow characteristics of the TLV cavitation were widely... The tip-leakage vortex(TLV)cavitation is a challenging issue for a variety of axial hydraulic turbines and pumps from both technical and scientific viewpoints.The flow characteristics of the TLV cavitation were widely studied in the past decades,but the knowledge about the tip-leakage cavitating flow is still limited.The present paper reviews the progresses in the researches of the TLV cavitation,including the numerical methods for the TLV cavitation,the flow characteristics of the TLV,the influences of the TLV cavitation on the local flow field and the control strategies of the TLV cavitation.It is indicated that the non-condensable gas may play an important role in the development of the TLV cavitation,and this fact should be considered during a careful simulation of the TLV cavitation.It is also suggested that the development of the TLV cavitation will significantly influence the distributions of the vorticity and the turbulence kinetic energy.Due to the complexity of the TLV cavitation,it is still an open question how to suppress the TLV cavitation in a simple but effective way.Finally,based on these understandings,some advanced topics for the future work are suggested to further promote the study of the TLV cavitation,for a deeper knowledge about the TLV cavitation. 展开更多
关键词 CAVITATION tip-leakage vortex(tlv) CAVITATION model flow CONTROL NUCLEI
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URANS simulations of the tip-leakage cavitating flow with verification and validation procedures 被引量:5
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作者 Huai-yu Cheng Xin-ping Long +2 位作者 Yun-zhi Liang Yun Long Bin Ji 《Journal of Hydrodynamics》 SCIE EI CSCD 2018年第3期531-534,共4页
In the present paper, the Vortex Identified Zwart-Gerber-Belamri(VIZGB) cavitation model coupled with the SST-CC turbulence model is used to investigate the unsteady tip-leakage cavitating flow induced by a NACA0009... In the present paper, the Vortex Identified Zwart-Gerber-Belamri(VIZGB) cavitation model coupled with the SST-CC turbulence model is used to investigate the unsteady tip-leakage cavitating flow induced by a NACA0009 hydrofoil. A qualitative comparison between the numerical and experimental results is made. In order to quantitatively evaluate the reliability of the numerical data, the verification and validation(V&V) procedures are used in the present paper. Errors of numerical results are estimated with seven error estimators based on the Richardson extrapolation method. It is shown that though a strict validation cannot be achieved, a reasonable prediction of the gross characteristics of the tip-leakage cavitating flow can be obtained. Based on the numerical results, the influence of the cavitation on the tip-leakage vortex(TLV) is discussed, which indicates that the cavitation accelerates the fusion of the TLV and the tip-separation vortex(TSV). Moreover, the trajectory of the TLV, when the cavitation occurs, is close to the side wall. 展开更多
关键词 CAVITATION computational fluid dynamics(CFD) tip-leakage vortextlv verification and validation(V&V)
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Effect of Tip-Blade Cutting on the Performance of Large Scale Axial Fan
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作者 尹超 胡骏 +1 位作者 严伟 张晨凯 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2015年第6期623-630,共8页
The effect of tip-blade cutting on the performance of a large scale axial fan was investigated using computational fluid dynamics(CFD)methods.Experiments verified the numerical simulations.The original fan was compare... The effect of tip-blade cutting on the performance of a large scale axial fan was investigated using computational fluid dynamics(CFD)methods.Experiments verified the numerical simulations.The original fan was compared with the one with tip-cutting in terms of dimensionless characteristic and aerodynamic performance in tip region under the conditions of the maximum efficiency point and near-stall point.The results showed that double leakage flow occurred in tip clearance at maximum efficiency point and spillage of leakage flow from leading edge occurred in tip-blade region at near-stall point for the both two fans;and that tip-cutting with 6% of blade height could reduce the intensity of tip-leakage vortex and increase flow capacity in tip blade region,and hold the stall margin almost the same as the original fan.The maximum efficiency of the fan with tip-cutting was improved by1%,and the ability of total pressure rising was obviously greater than the original fan. 展开更多
关键词 large axial fan tip-blade cutting numerical simulation tip-leakage vortex flow capacity
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Research on blade tip clearance cavitation and turbulent kinetic energy characteristics of axial flow pump based on the partially-averaged Navier-Stokes model
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作者 Xiao-qi Jia Shuai-kang Zhang Zu-chao Zhu 《Journal of Hydrodynamics》 SCIE EI CSCD 2024年第1期184-201,共18页
To reveal the cavitation forms of tip leakage vortex(TLV)of the axial flow pump and the flow mechanism of the flow field,this research adopts the partially-averaged Navier-Stokes(PANS)model to simulate the cavitation ... To reveal the cavitation forms of tip leakage vortex(TLV)of the axial flow pump and the flow mechanism of the flow field,this research adopts the partially-averaged Navier-Stokes(PANS)model to simulate the cavitation values of an axial flow pump,followed by experimental validation.The experimental result shows that compared with the shear stress transport(SST)k-ωmodel,the PANS model significantly reduces the eddy viscosity of the flow field to make the vortex structure clearer and allow the turbulence scale to be more robustly analyzed.The cavitation area within the axial flow pump mainly comprises of TLV cavitation,clearance cavitation and tip leakage flows combined effect of triangular cloud cavitation formed.The formation and development of cavitation are accompanied by the formation and evolution of vortex,and variations in vortex structure also generate and promote the development of cavitation.In addition,an in-depth analysis of the relationship between the turbulent kinetic energy(TKE)transport equation and cavitation patterns was also conducted,finding that the regions with relatively high TKE are mainly distributed around gas/liquid boundaries with serious cavitation and evident gas-liquid change.This phenomenon is mainly attributed to the combined effect of the pressure action term,stress diffusion term and TKE production term. 展开更多
关键词 CAVITATION axial flow pump tip leakage vortex(tlv) partially-averaged Navier-Stokes(PANS)model turbulent kinetic energy(TKE)
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Large eddy simulation of tip leakage cavitating flow focusing on cavitation-vortex interaction with Cartesian cut-cell mesh method 被引量:2
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作者 白晓蕊 程怀玉 +1 位作者 季斌 龙新平 《Journal of Hydrodynamics》 SCIE EI CSCD 2018年第4期750-753,共4页
In the present paper, flow configurations of cavitating flow around a straight NACA0009 foil with a gap between the foil tip and sidewall are investigated numerically by large eddy simulation(LES) coupled with Zwart... In the present paper, flow configurations of cavitating flow around a straight NACA0009 foil with a gap between the foil tip and sidewall are investigated numerically by large eddy simulation(LES) coupled with Zwart-Gerber-Belamri(ZGB) cavitation model. A Cartesian cut-cell method is used for mesh generation, which is of good orthogonality and high quality. A good agreement is obtained between simulation and experiment. Two influencing factors on vorticity distributions, the interaction between different vortices and the occurrence of cavitation, are discussed in detail based on the numerical results. A series of ?-shaped loops are observed during the development of the induced vortex, which is a result of the instability of vortex pair. This finding may provide a new viewpoint to control the evolution of tip-leakage vortex(TLV) cavitation. Moreover, it is found that the dilatation term plays a much more important role in the evolution of TLV cavitation compared with that in sheet cavitation. 展开更多
关键词 CAVITATION tip-leakage vortex large eddy simulation (LES) Cartesian cut-cell mesh vortex dynamics
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激波/泄漏涡相互干扰对跨声压气机流动稳定性的影响 被引量:11
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作者 张卓勋 吴艳辉 +1 位作者 楚武利 张皓光 《航空动力学报》 EI CAS CSCD 北大核心 2010年第7期1615-1621,共7页
对单级跨声压气机Stage 35进行了单通道全三维定常数值模拟,开展了网格密度对计算结果影响的研究,从而确定了一套最佳网格配置,该套网格配置预测的总性能和基元性能与试验结果符合得最好.以此为基础对Stage 35的内部流场进行分析,发现... 对单级跨声压气机Stage 35进行了单通道全三维定常数值模拟,开展了网格密度对计算结果影响的研究,从而确定了一套最佳网格配置,该套网格配置预测的总性能和基元性能与试验结果符合得最好.以此为基础对Stage 35的内部流场进行分析,发现其流动失稳最有可能是由动叶近叶顶靠近压力面侧的低能堵塞团引发的.随着流量的减小,间隙泄漏涡的强度和旋拧度随着叶片载荷的增加而增加,激波与泄漏涡相互干扰使得近失速条件下间隙泄漏涡破碎,涡破碎极有可能是动叶近叶顶靠近压力面侧低能流体产生的主要原因. 展开更多
关键词 跨声速 数值模拟 流动稳定性 激波 间隙泄漏涡
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跨声轴流压气机激波/泄漏涡/边界层分离相互作用的影响 被引量:25
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作者 谢芳 楚武利 张皓光 《航空动力学报》 EI CAS CSCD 北大核心 2012年第2期425-430,共6页
对跨声速转子Rotor37进行三维定常数值模拟,将设计间隙与零间隙进行对比研究,分析激波、边界层分离、间隙泄漏涡相互作用影响.数值计算显示:激波、泄漏涡、边界层分离相互影响,加速了失速的发生;减小间隙可以起到扩稳的作用.根据边界层... 对跨声速转子Rotor37进行三维定常数值模拟,将设计间隙与零间隙进行对比研究,分析激波、边界层分离、间隙泄漏涡相互作用影响.数值计算显示:激波、泄漏涡、边界层分离相互影响,加速了失速的发生;减小间隙可以起到扩稳的作用.根据边界层分离、间隙泄漏涡在叶栅高度上的影响范围,提出利用抽吸技术进行被动控制改善流道流动状况时抽吸点的设置位置. 展开更多
关键词 跨声速 轴流压气机 激波 间隙泄漏涡 边界层分离
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跨声速风扇转子间隙流动结构分析 被引量:6
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作者 杨晰琼 刘波 +2 位作者 曹志远 茅晓晨 夏树丹 《航空动力学报》 EI CAS CSCD 北大核心 2016年第9期2258-2267,共10页
为探索跨声速转子间隙流动结构,归纳间隙泄漏涡(TLV)和激波相互作用机理,以跨声速转子为研究对象,数值模拟不同间隙下流动特性.此外,着重探究TLV与激波的相互作用,斜激波受到间隙泄漏流的干扰,被削弱打断向上游凹曲;建立三维模型,加深... 为探索跨声速转子间隙流动结构,归纳间隙泄漏涡(TLV)和激波相互作用机理,以跨声速转子为研究对象,数值模拟不同间隙下流动特性.此外,着重探究TLV与激波的相互作用,斜激波受到间隙泄漏流的干扰,被削弱打断向上游凹曲;建立三维模型,加深对跨声速叶尖区域流动的全面认识.研究表明:随间隙增大,相同流量下,效率越小,压比也越小;TLV强度更大,偏离吸力面程度增大,沿周向和展向影响范围都越大.压力差提供泄漏流迁移动力,间隙提供泄漏流形成通道.选取h/c=1.0%间隙,随着间隙高度的增大,泄漏流周向运动趋势更明显且二次泄漏现象更剧烈;沿泄漏流方向无量纲流向涡量有少量减少,无量纲螺旋度较高,集中涡特性明显. 展开更多
关键词 跨声速 间隙泄漏涡 流动结构 激波 相互作用
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Pressure fluctuation characteristics in the pressurization unit of a multiphase pump 被引量:1
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作者 Guang-tai Shi Zong-ku Liu +2 位作者 Ye-xiang Xiao Xue-lin Tang Xiao-bing Liu 《Journal of Hydrodynamics》 SCIE EI CSCD 2021年第6期1230-1241,共12页
The tip clearance induces the tip leakage vortex(TLV),which has a great impact on the pressure fluctuation characteristics of the multiphase pump.To investigate the effect of the tip clearance on the pressure fluctuat... The tip clearance induces the tip leakage vortex(TLV),which has a great impact on the pressure fluctuation characteristics of the multiphase pump.To investigate the effect of the tip clearance on the pressure fluctuations,based on the Reynolds time-averaged Navier-Stokes equation and the shear stress transfer(SST)k-ωturbulence model,the three-dimensional turbulent flow in the pump is numerically simulated for different tip clearances in the water and gas-liquid two-phase cases by using the ANSYS CFX software and the results are verified with experimental data.It is shown the greater pressure fluctuation intensity corresponds with the TLV both in the water and gas-liquid two-phase cases.In the meantime,the location of the maximum pressure fluctuation intensity is related to the tip clearance size.In addition,for different tip clearances,the pressure fluctuation intensity with the rotor and stator interaction(RSI)is relatively larger.The difference is that when R_(tc)=1.5 mm,the pressure fluctuation intensity near the impeller middle point is also relatively larger.On the whole,the pressure fluctuation intensity in the gas-liquid two-phase case is larger than that in the water case.Furthermore,the gas causes the frequency of the high-amplitude pressure fluctuation in the impeller and the diffuser to be shifted from 7 f_(n)(f_(n) denotes impeller rotational frequency)and 3 f_(n) to the low-frequency region,respectively.The pressure fluctuations at the blade-passing frequency(BPF)and the multiple BPFs gradually disappear.Meanwhile,the amplitude at the dominant frequency in the gas-liquid two-phase case is at least one order of magnitude smaller than that in the water case,and the peak-to-peak value of the pressure fluctuation is also much smaller. 展开更多
关键词 Multiphase pump gas void faction pressure fluctuation intensity tip leakage vortex(tlv) numerical simulation
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