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基于自适应网格技术的Clark-Y水翼空泡数值模拟 被引量:5
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作者 梁尚 李勇 万德成 《水动力学研究与进展(A辑)》 CSCD 北大核心 2020年第1期1-8,共8页
空化流动具有高度非定常性,界面模糊而且处于不断地形变之中。该研究基于开源的CFD平台OpenFOAM,利用interPhaseChangeDyMFoam求解器对Clark-Y水翼的空泡流进行数值模拟,并利用自适应网格技术对空化区域尤其是两相界面附近的网格进行了... 空化流动具有高度非定常性,界面模糊而且处于不断地形变之中。该研究基于开源的CFD平台OpenFOAM,利用interPhaseChangeDyMFoam求解器对Clark-Y水翼的空泡流进行数值模拟,并利用自适应网格技术对空化区域尤其是两相界面附近的网格进行了局部加密,考察并分析了水翼的水动力性能和空泡形态。文中将模拟结果与试验结果相比较,发现通过自适应网格加密可以有效捕捉空泡形态的变化尤其是片空泡脱落过程和云空泡溃灭过程。研究表明,针对空化区域的自适应网格加密能够在计算量一定的情况下有效提高空泡流模拟精度。 展开更多
关键词 OPENFOAM 空泡流 自适应网格 clark-y水翼
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Numerical Simulations of Cavitation Flows around Clark-Y Hydrofoil 被引量:3
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作者 Yijie Liu Jianhua Wang Decheng Wan 《Journal of Applied Mathematics and Physics》 2019年第8期1660-1676,共17页
Cavitation is a complex flow phenomenon including unsteady characteristics, turbulence, gas-liquid two-phase flow. This paper provides a numerical investigation on comparing the simulation performance of three differe... Cavitation is a complex flow phenomenon including unsteady characteristics, turbulence, gas-liquid two-phase flow. This paper provides a numerical investigation on comparing the simulation performance of three different models in OpenFOAM-Merkle model, Kunz model and Schnerr-Sauer model, which is helpful for understanding the cavitation flow. Considering the influence of vapor-liquid mixing density on turbulent viscous coefficient, the modified SST k-ω model is adopted in this paper to increase the computing reliability. The InterPhaseChangeFoam solver is utilized to simulate the two-dimensional cavitation flow of the Clark-Y hydrofoil with three cavitation models. The hydrodynamic performance including lift coefficient, drag coefficient and cavitation flow shape of the hydrofoil is analyzed. Through the comparison of the numerical results and experimental data, it is found that the Schnerr-Sauer model can get the most accurate results among the three models. And from the simulation point of water and water vapor mixing, the Merkle model has the best water and water vapor mixing simulation. 展开更多
关键词 CAVITATION Flow OPENFOAM Modified SST k-ω Model clark-y HYDROFOIL
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Numerical Investigation of the Angle of Attack Effect on Cloud Cavitation Flow around a Clark-Y Hydrofoil
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作者 Di Peng Guoqing Chen +1 位作者 Jiale Yan Shiping Wang 《Computer Modeling in Engineering & Sciences》 SCIE EI 2024年第6期2947-2964,共18页
Cavitation is a prevalent phenomenon within the domain of ship and ocean engineering,predominantly occurring in the tail flow fields of high-speed rotating propellers and on the surfaces of high-speed underwater vehic... Cavitation is a prevalent phenomenon within the domain of ship and ocean engineering,predominantly occurring in the tail flow fields of high-speed rotating propellers and on the surfaces of high-speed underwater vehicles.The re-entrant jet and compression wave resulting from the collapse of cavity vapour are pivotal factors contributing to cavity instability.Concurrently,these phenomena significantly modulate the evolution of cavitation flow.In this paper,numerical investigations into cloud cavitation over a Clark-Y hydrofoil were conducted,utilizing the Large Eddy Simulation(LES)turbulence model and the Volume of Fluid(VOF)method within the OpenFOAM framework.Comparative analysis of results obtained at different angles of attack is undertaken.A discernible augmentation in cavity thickness is observed concomitant with the escalation in attack angle,alongside a progressive intensification in pressure at the leading edge of the hydrofoil,contributing to the suction force.These results can serve as a fundamental point of reference for gaining a deeper comprehension of cloud cavitation dynamics. 展开更多
关键词 Cloud cavitation re-entrant jet compression wave clark-y hydrofoil
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二维Clark-Y水翼云空化球形空泡动力学特性
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作者 洪锋 郭泽霖 +5 位作者 袁喜 刘书畅 黄笛 贾金平 雷恩宏 黄应平 《排灌机械工程学报》 2026年第2期148-155,共8页
为了研究云空化周期性演变过程中的空泡动力学特性,基于均相流模型与离散相模型构建了一种单向耦合欧拉-拉格朗日思想的水力空化模拟方法,对空化数σ=0.8的二维Clark-Y水翼云空化流动进行了数值计算,得到了水翼瞬时升力系数变化及其表... 为了研究云空化周期性演变过程中的空泡动力学特性,基于均相流模型与离散相模型构建了一种单向耦合欧拉-拉格朗日思想的水力空化模拟方法,对空化数σ=0.8的二维Clark-Y水翼云空化流动进行了数值计算,得到了水翼瞬时升力系数变化及其表面云空化演变过程.通过求解球形空泡动力学方程,获取了该水翼云空化区内的空泡动力学演变规律.研究结果表明:该数值方法较好地模拟了水翼云空化内空泡的周期性行为;示踪粒子沿途压力的剧烈程度受空泡脱落与溃灭位置的影响;空泡内压与其所受流场压力有关,流场压力变化越剧烈,空泡内压幅值越高,其溃灭所释放的压力波也就越大,当空泡半径收缩至15.7μm时其溃灭压强最大幅值可达69.800 MPa;空泡初始半径增大,空泡内压幅值随之减小,空泡形态变化基本稳定.文中研究方法可为大型水力机械中的球形空泡溃灭行为研究提供理论参考. 展开更多
关键词 云空化 空泡动力学 clark-y水翼 大涡模拟 单向耦合
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3-D Lagrangian-based investigations of the time-dependent cloud cavitating flows around a Clark-Y hydrofoil with special emphasis on shedding process analysis 被引量:4
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作者 程怀玉 龙新平 +2 位作者 季斌 刘琦 白晓蕊 《Journal of Hydrodynamics》 SCIE EI CSCD 2018年第1期122-130,共9页
In the present paper, the unsteady cavitating flow around a 3-D Clark-Y hydrofoil is numerically investigated with the filter-based density correction model(FBDCM), a turbulence model and the Zwart-Gerber-Belamri(... In the present paper, the unsteady cavitating flow around a 3-D Clark-Y hydrofoil is numerically investigated with the filter-based density correction model(FBDCM), a turbulence model and the Zwart-Gerber-Belamri(ZGB) cavitation model. A reasonable agreement is obtained between the numerical and experimental results. To study the complex flow structures more straightforwardly, a 3-D Lagrangian technology is developed, which can provide the particle tracks and the 3-D Lagrangian coherent structures(LCSs). Combined with the traditional methods based on the Eulerian viewpoint, this technology is used to analyze the attached cavity evolution and the re-entrant jet behavior in detail. At stage I, the collapse of the previous shedding cavity and the growth of a new attached cavity, the significant influence of the collapse both on the suction and pressure sides are captured quite well by the 3-D LCSs, which is underestimated by the traditional methods like the iso-surface of Q-criteria. As a kind of special LCSs, the arching LCSs are observed in the wake, induced by the counter-rotating vortexes. At stage II, with the development of the re-entrant jet,the influence of the cavitation on the pressure side is still not negligible. And with this 3-D Lagrangian technology, the tracks of the re-entrant jet are visualized clearly, moving from the trailing edge to the leading edge. Finally, at stage Ⅲ, the re-entrant jet collides with the mainstream and finally induces the shedding. The cavitation evolution and the re-entrant jet movement in the whole cycle are well visualized with the 3-D Lagrangian technology. Moreover, the comparison between the LCSs obtained with 2-D and 3-D Lagrangian technologies indicates the advantages of the latter. It is demonstrated that the 3-D Lagrangian technology is a promising tool in the investigation of complex cavitating flows. 展开更多
关键词 Cavitation CFD Lagrangian coherent structures(LCSs) clark-y hydrofoil vortical flow
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考虑当地流动特征的Zwart-Gerbera-Belamri空化模型改进及应用 被引量:5
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作者 胡俊 侯夏伊 于勇 《北京理工大学学报》 EI CAS CSCD 北大核心 2021年第4期388-394,共7页
为减小Zwart-Gerbera-Belamri空化模型中经验参数取值对数值模拟结果的影响,基于当地流动特征修正了Zwart-Gerbera-Belamri空化模型.联立Realizable k-ε湍流模型,分别采用修正前后的Zwart-Gerbera-Belamri空化模型对二维NACA0009 MOD... 为减小Zwart-Gerbera-Belamri空化模型中经验参数取值对数值模拟结果的影响,基于当地流动特征修正了Zwart-Gerbera-Belamri空化模型.联立Realizable k-ε湍流模型,分别采用修正前后的Zwart-Gerbera-Belamri空化模型对二维NACA0009 MOD水翼空化流场进行了数值模拟,空化数范围为0.75~0.90.并采用修正前后的Zwart-Gerbera-Belamri空化模型对二维Clark-Y水翼的初生空化、片状空化、云空化进行非定常数值模拟,空化数范围为3.00~0.55.将数值模拟结果与已有实验结果进行对比,结果表明:引入当地流动特征可以有效减小Zwart-Gerbera-Belamri空化模型中的气泡半径及气核体积分数的取值对数值模拟结果的影响,且修正后的空化模型能够捕捉不同空化数下绕Clark-Y翼型的时均升阻力系数的变化趋势. 展开更多
关键词 数值模拟 NACA0009水翼 clark-y水翼 Zwart-Gerbera-Belamri空化模型
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某二维水翼空化数值模型对比研究 被引量:1
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作者 蒋文青 郑源 葛新峰 《南水北调与水利科技》 CSCD 北大核心 2017年第3期204-208,共5页
以二维水翼计算模型为研究对象,采用数值模拟的方法,通过不同的空化模型和湍流模型对计算模型进行数值模拟研究,得到了翼型在空化过程中空泡的运动规律。结果表明:该翼型在不同空化模型下,发生空化时,空化过程包含了空泡的产生、发展、... 以二维水翼计算模型为研究对象,采用数值模拟的方法,通过不同的空化模型和湍流模型对计算模型进行数值模拟研究,得到了翼型在空化过程中空泡的运动规律。结果表明:该翼型在不同空化模型下,发生空化时,空化过程包含了空泡的产生、发展、脱落和溃灭几个过程,空化的运动过程总具有明显的周期性;Schnerr-Sauer模型的计算结果与实际的水翼空化流动过程相吻合,Schnerr-Sauer空化模型可以很好地模拟绕水翼的空化流动过程。 展开更多
关键词 clark-y翼型 空化 数值模拟 空泡 运动规律
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一种基于CST技术的机翼参数化描述方法 被引量:2
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作者 闫博文 黄俊 +1 位作者 刘志勤 王耀彬 《导弹与航天运载技术》 CSCD 北大核心 2019年第1期101-104,共4页
为了确保翼型性能,需要采用恰当的翼型参数化方法生成所需要的翼型几何体。利用CST方法生成具有代表性的Clark-Y二维机翼,同时对CST方法生成三维几何体进行了详细研究。在原有的CST方法基础上对生成三维机翼的方法进行改进,用来解决机... 为了确保翼型性能,需要采用恰当的翼型参数化方法生成所需要的翼型几何体。利用CST方法生成具有代表性的Clark-Y二维机翼,同时对CST方法生成三维几何体进行了详细研究。在原有的CST方法基础上对生成三维机翼的方法进行改进,用来解决机翼外形不连续变化的情况,生成可控分段变化三维机翼外形,控制效果良好。 展开更多
关键词 CST参数化方法 类别函数 形状函数 clark-y二维机翼
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基于Clark Y的非对称翼型对可逆轴流风机性能影响的研究 被引量:8
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作者 王海民 高涌东 +1 位作者 胡峰 陈思 《热能动力工程》 CAS CSCD 北大核心 2020年第1期83-90,105,共9页
针对双向通风机的工程应用,基于Clark Y标准翼型采用尾部反接法设计了4种"S"型非对称翼型(反接段弦长与总弦长的占比分别为0.286、0.375、0.444和0.500),并应用至单级可逆轴流风机,通过数值模拟及风机性能试验对比分析4种可... 针对双向通风机的工程应用,基于Clark Y标准翼型采用尾部反接法设计了4种"S"型非对称翼型(反接段弦长与总弦长的占比分别为0.286、0.375、0.444和0.500),并应用至单级可逆轴流风机,通过数值模拟及风机性能试验对比分析4种可逆翼型的风机在双向来流中气动性能。研究表明:随着前缘厚度增加,风机进口截面的和叶顶间隙的湍流动能会有所下降,减小了流动损失,而增加尾缘最大厚度会降低叶轮出口流通性能;反映到风机的性能上,增加前缘最大厚度同时减小尾缘最大厚度,风机正向通风时效率及全压会有所下降,而反向通风时两者均有大幅提升;采用反接段弦长占比为0.444的非对称翼型风机整体性能较优。 展开更多
关键词 Clark Y翼型 非对称翼型 可逆轴流风机 流场分布 性能试验
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利用Clark Y构造非对称翼型风机的正向通风性能对比 被引量:5
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作者 王海民 高涌东 +1 位作者 胡峰 陈思 《流体机械》 CSCD 北大核心 2020年第1期46-52,共7页
针对双向通风的工程应用,基于Clark Y标准翼型设计了4种S型非对称翼型并应用至单级可逆轴流风机,通过数值模拟计算及性能试验分析,对比研究了采用不同S翼型的可逆风机仅在正向通风情况下的气动性能。数值模拟结果表明:随着前缘厚度增加... 针对双向通风的工程应用,基于Clark Y标准翼型设计了4种S型非对称翼型并应用至单级可逆轴流风机,通过数值模拟计算及性能试验分析,对比研究了采用不同S翼型的可逆风机仅在正向通风情况下的气动性能。数值模拟结果表明:随着前缘厚度增加,风机进口截面的和叶顶间隙的湍流动能会有所下降,减少了流动损失,而增加尾缘最大厚度会降低叶轮出口流通性能。因此,反映到风机的性能上,在满足逆向通风的流量和静压前提下,增加前缘最大厚度同时减少尾缘最大厚度,风机正向通风时效率及全压会随之发生下降。综合比较而言,本文所研究的运用在正向吹风工况中的4类可逆风机,其中F4性能较优,而F10性能相对最差。 展开更多
关键词 Clark Y翼型 非对称翼型 可逆风机 正向吹风 流场分布 性能试验
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中国嵩草属新分类群 被引量:3
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作者 李沛琼 《植物分类学报》 CSCD 1999年第2期153-155,共3页
1粉绿嵩草新种图1KobresiaglaucifoliaWangetTang,inherb.,sp.nov.(Sect.Elyna).Fig.1AfinisK.cuneataeKükenth.,quaeinflo... 1粉绿嵩草新种图1KobresiaglaucifoliaWangetTang,inherb.,sp.nov.(Sect.Elyna).Fig.1AfinisK.cuneataeKükenth.,quaeinflorescentisad9~12mmcr... 展开更多
关键词 嵩草属 粉绿嵩草 匍茎嵩草 近蕨嵩草 菊科
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Numerical analysis of cavitation shedding flow around a three-dimensional hydrofoil using an improved filter-based model 被引量:2
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作者 张德胜 施卫东 +2 位作者 张光建 陈健 B.P.M.(Bart)van Esch 《Journal of Hydrodynamics》 SCIE EI CSCD 2017年第2期361-375,共15页
The cavitation shedding flow around a 3-D Clark-Y hydrofoil is simulated by using an improved filter-based model (FBM) and a mass transfer cavitation model with the consideration of the maximum density ratio effect ... The cavitation shedding flow around a 3-D Clark-Y hydrofoil is simulated by using an improved filter-based model (FBM) and a mass transfer cavitation model with the consideration of the maximum density ratio effect between the liquid and the vapor. The unsteady cloud cavity shedding features around the Clark-Y hydrofoil are accurately captured based on an improved FBM model and a suitable maximum density ratio. Numerical results show that the predicted cavitation patterns and evolutions compare well with the experimental visualizations, and the prediction errors of the time-averaged lift coefficient, drag coefficient and Strouhal number St for the cavitation number o- = 0.8, the angle of attack a= 8°at a Reynolds number Re = 7 x 10^5 are only 3.29%, 2.36% and 9.58%, respectively. It is observed that the cavitation shedding flow patterns are closely associated with the vortex structures identified by the Q- criterion method. The predicted cloud cavitation shedding flow shows clearly three typical stages: (1) Initiation of the attached sheet cavity, the growth toward the trailing edge. (2) The formation and development of the re-entrant jet flow. (3) Large scale cloud cavity sheds downstream. Numerical results also indicate that the non-uniform adverse pressure gradient is the main driving force of the re-entrant jet, which results in the U-shaped cavity and the 3-D bubbly structure during the cloud cavity shedding. 展开更多
关键词 Cloud cavitation shedding flow filter-based model turbulent viscosity clark-y hydrofoil
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