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修正的RNG κ-ε模型在云状空化流动计算中的应用评价 被引量:24
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作者 张博 王国玉 +1 位作者 张淑丽 余志毅 《北京理工大学学报》 EI CAS CSCD 北大核心 2008年第12期1065-1069,共5页
基于实验结果评价了一种用密度函数修正的RNGκ-ε湍流模型在云状空化流动计算中的应用.采用不同的修正系数,分别计算了绕Clark-y型水翼云状空化流动,获得了随时间变化的空化形态和升、阻力等流场及动力特性.通过与实验结果的对比表明,... 基于实验结果评价了一种用密度函数修正的RNGκ-ε湍流模型在云状空化流动计算中的应用.采用不同的修正系数,分别计算了绕Clark-y型水翼云状空化流动,获得了随时间变化的空化形态和升、阻力等流场及动力特性.通过与实验结果的对比表明,修正后的模型可以更准确地捕捉云状空化区域的空穴形态和空泡脱落的非定常细节;密度函数中指数n的选取对计算所得的空穴长度和升阻力均有影响,然而对流场动力特性的主要频谱分布影响不明显. 展开更多
关键词 湍流模型 云状空化 脱落频率
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云状空化非定常脱落机理的数值与实验研究 被引量:21
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作者 张博 王国玉 +1 位作者 黄彪 余志毅 《力学学报》 EI CSCD 北大核心 2009年第5期651-659,共9页
结合数值计算和实验技术研究了云状空化的非定常脱落机理.实验采用高速录像技术观察了绕Clark-y型水翼云状空化形态随时间的变化.数值计算采用了汽-液两相的当地均相流模型,湍流封闭采用了一种修正的RNG k-ε方程,利用商业软件的二次开... 结合数值计算和实验技术研究了云状空化的非定常脱落机理.实验采用高速录像技术观察了绕Clark-y型水翼云状空化形态随时间的变化.数值计算采用了汽-液两相的当地均相流模型,湍流封闭采用了一种修正的RNG k-ε方程,利用商业软件的二次开发技术,引入了一种与空化区域水汽相密度相关的系数,对湍流模型进行了修正.计算和实验结果均表明:云状空化尾部存在着准周期性的涡状空化团的脱落;局部压强的增加是引起空穴断裂进而脱落的直接原因;压强升高是由于近壁处的反向射流引起的;空穴尾部的大规模的旋涡运动引起的近壁处的逆压梯度是引起反向射流的主要原因. 展开更多
关键词 云状空化 均相流模型 湍流模型 反向射流 逆压梯度
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基于k-ωSST模型的DES方法在空化流动计算中的应用 被引量:14
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作者 黄彪 王国玉 《中国机械工程》 EI CAS CSCD 北大核心 2010年第1期85-89,共5页
基于试验结果评价了基于k-ωSST两个方程的DES湍流模型在空化流动中的应用,分别计算了绕Clark-y型水翼云状空化与Hydronautics型水翼超空化流动,获得了随时间变化的空穴形态与流场结构细节。通过与试验结果对比发现,DES方法对于高雷诺... 基于试验结果评价了基于k-ωSST两个方程的DES湍流模型在空化流动中的应用,分别计算了绕Clark-y型水翼云状空化与Hydronautics型水翼超空化流动,获得了随时间变化的空穴形态与流场结构细节。通过与试验结果对比发现,DES方法对于高雷诺数的绕水翼空化流动的预测是合理的,可以准确地模拟出空穴形态的非定常特性和空泡团交替脱落的非定常细节。 展开更多
关键词 DES湍流模型 云状空化 超空化 非定常特性
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On the numerical simulations of vortical cavitating flows around various hydrofoils 被引量:10
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作者 王本龙 刘志辉 +4 位作者 李颢钰 王雅赟 刘登成 张凌新 彭晓星 《Journal of Hydrodynamics》 SCIE EI CSCD 2017年第6期926-938,共13页
This paper reviews the numerical models of various cavitating flows around hydrofoils. Numerical models relating to cavitation flows, including mass transfer models and turbulence models, are summarized at first. Then... This paper reviews the numerical models of various cavitating flows around hydrofoils. Numerical models relating to cavitation flows, including mass transfer models and turbulence models, are summarized at first. Then numerical results and analysis of flow characteristics for the cavitating flows around twisted hydrofoils, truncated hydrofoil and tip leakage are discussed respectively. For mean flow fields, Reynolds averaged Navier-Stokes(RANS) simulation associated with a kind of nonlinear turbulence model is found to be an economic and robust numerical approach for different kinds of cavitating flows including cloud cavitation, tip cavitation and tip leakage cavitation. To predict the fluctuations of pressure and velocity, large eddy simulation(LES) and detached eddy simulation(DES) are two effective approaches. Finally, a few open questions are proposed for future research. 展开更多
关键词 Mass transfer model turbulence model sheet cavitation cloud cavitation tip cavitation
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离心泵非定常空化流动特性的数值研究 被引量:13
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作者 刘春哲 王国光 +1 位作者 尹光志 田辉 《流体机械》 CSCD 北大核心 2019年第7期39-43,26,共6页
采用压力边界条件对一单级单吸蜗壳离心泵进行了三维空化非定常相变流动的数值计算,模拟过程通过定常计算、基于滑移网格技术的非定常计算、以及结合混合项模型和Schneer-Sauer方程的空化演变计算,成功捕捉了泵内非定常空化流动特性。... 采用压力边界条件对一单级单吸蜗壳离心泵进行了三维空化非定常相变流动的数值计算,模拟过程通过定常计算、基于滑移网格技术的非定常计算、以及结合混合项模型和Schneer-Sauer方程的空化演变计算,成功捕捉了泵内非定常空化流动特性。计算结果表明:设计工况叶轮前缘空化率在0.92%~1.12%范围内以叶片旋转频率做周期性变化;当叶片靠近蜗舌时空化加剧,而泵流量略有降低;当叶片远离蜗舌时空化减轻,流量有所增加。 展开更多
关键词 离心泵 非定常 附着空化 云空化 数值模拟
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水下回转航行体的云状空化回射流运动特征研究 被引量:13
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作者 王一伟 黄晨光 +2 位作者 方新 杜特专 于娴娴 《水动力学研究与进展(A辑)》 CSCD 北大核心 2013年第1期23-29,共7页
该文针对典型的细长回转航行体的水下航行过程,基于SHPB(霍普金森压杆)发射系统开展了机理性实验。相应基于单一流体/多相混合模型,结合空化模型及修正的RNG k湍流模式对该问题进行了数值模拟。并在实验与数值模拟结果的基础上,研究了... 该文针对典型的细长回转航行体的水下航行过程,基于SHPB(霍普金森压杆)发射系统开展了机理性实验。相应基于单一流体/多相混合模型,结合空化模型及修正的RNG k湍流模式对该问题进行了数值模拟。并在实验与数值模拟结果的基础上,研究了回射流诱导的云状空化不稳定性问题,探讨了该现象中空化非稳态演化的物理机制,分析了空泡末端回射流的产生原因以及它对空泡演化的诱导作用。进一步从压力梯度角度给出了回射流运动的动力学模型和空泡长度的预测表达式,并通过数值结果验证了该模型和公式的有效性。 展开更多
关键词 云状空化 回转体 回射流模型 逆压梯度
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云状空化流动数值模拟的空化模型评价 被引量:10
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作者 黄彪 王国玉 +1 位作者 张博 余志毅 《北京理工大学学报》 EI CAS CSCD 北大核心 2009年第9期785-789,共5页
为深入了解空化模型对云状空化流动计算的影响,分别采用Kubota,Singhal,Merkle,Kunz四种不同的空化模型对绕水翼的云状空化流动进行了数值模拟,获得了空穴形态和升、阻力等流场动力随时间的变化特性.通过与实验结果的对比表明,这四种空... 为深入了解空化模型对云状空化流动计算的影响,分别采用Kubota,Singhal,Merkle,Kunz四种不同的空化模型对绕水翼的云状空化流动进行了数值模拟,获得了空穴形态和升、阻力等流场动力随时间的变化特性.通过与实验结果的对比表明,这四种空化模型均可以准确地捕捉云状空化区域的空穴形态和空泡脱落的非定常细节;不同空化模型对计算所得的空穴形态和长度、绕翼型速度矢量场、升阻力均有影响,但对流场动力特性的主要频谱分布影响不大. 展开更多
关键词 云状空化 空化模型 数值计算
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基于不同空化模型NACA66水翼三维空化特性数值研究 被引量:12
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作者 郑小波 刘莉莉 +1 位作者 郭鹏程 洪锋 《水动力学研究与进展(A辑)》 CSCD 北大核心 2018年第2期199-206,共8页
为了比较Zwart-Gerber-Belamri(ZGB)空化模型、Schnerr-Sauer(S-S)空化模型和改进后的Schnerr-Sauer(S-S)空化模型对水翼空化流动数值计算的影响,该文以攻角为6°的NACA66型三维水翼为研究对象,基于密度修正(DCM)的SST k-ω湍流模型... 为了比较Zwart-Gerber-Belamri(ZGB)空化模型、Schnerr-Sauer(S-S)空化模型和改进后的Schnerr-Sauer(S-S)空化模型对水翼空化流动数值计算的影响,该文以攻角为6°的NACA66型三维水翼为研究对象,基于密度修正(DCM)的SST k-ω湍流模型,采用湍动能修正后的空化模型并对其非定常空化流场进行数值计算。获得了不同空化模型计算得到的翼型升阻力系数、吸力面空泡形态演变、速度场的分布规律以及翼型表面平均压力分布规律。结果表明,在非稳定空化状态下,ZGB和改进后的S-S均模拟出非定常空化的准周期性,而原始S-S预测非定常准周期性不明显。三种空化模型均捕捉到空化流场中的回射流结构,ZGB模型和改进后的S-S模型较原始S-S模型能捕捉到更强烈的云状空化,且空化向尾缘发展,随后向下游脱落,这与已有文献中的实验结果基本一致。 展开更多
关键词 云状空化 NACA66水翼 空化模型 回射流 数值计算
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水翼表面布置射流水孔抑制空化 被引量:9
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作者 王巍 羿琦 +2 位作者 林茵 徐瑞铎 王晓放 《排灌机械工程学报》 EI CSCD 北大核心 2016年第10期872-877,共6页
为研究水翼表面布置射流水孔对空化的抑制效果,采用RNG k-ε湍流模型结合全空化模型对8°攻角NACA0066(MOD)水翼进行二维非定常空化流场计算,分析当射流比分别为0.1,0.2和0.3时的水翼表面空化流场结构及其演化过程的流动特性,得到... 为研究水翼表面布置射流水孔对空化的抑制效果,采用RNG k-ε湍流模型结合全空化模型对8°攻角NACA0066(MOD)水翼进行二维非定常空化流场计算,分析当射流比分别为0.1,0.2和0.3时的水翼表面空化流场结构及其演化过程的流动特性,得到了不同射流条件下水翼升阻力系数的变化趋势.计算结果表明:布置射流水孔可以有效阻挡回射流从翼型尾部向翼型头部的运动,使得空泡脱落现象明显减弱,从而抑制了片空化向云空化的发展,且随射流比增加,射流对回射流和云空化的抑制作用更加显著;射流的注入同时使得升力系数和阻力系数的波动幅度明显降低,有效减弱了升阻力的周期性振荡;虽然时均升力和时均阻力受射流的影响有下降趋势,但升阻比呈上升趋势,水翼升阻比由无射流孔时的6.11增加到射流比为0.3时的7.06,布置射流孔还起到了减阻的作用. 展开更多
关键词 水翼 射流比 云空化 空化抑制 升阻比
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High Speed Observation of Periodic Cavity Behavior in a Convergent-Divergent Nozzle for Cavitating Water Jet 被引量:8
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作者 Keiichi Sato Yuta Taguchi Shota Hayashi 《Journal of Flow Control, Measurement & Visualization》 2013年第3期102-107,共6页
Cloud cavitation shows an unsteady periodic tendency under a certain flow condition. In a cavitating water jet flow with cavitation clouds, the cavities or the clouds produce high impact at their collapse. In order to... Cloud cavitation shows an unsteady periodic tendency under a certain flow condition. In a cavitating water jet flow with cavitation clouds, the cavities or the clouds produce high impact at their collapse. In order to make clear a mechanism of the periodic cavity behavior, we experimentally examine the behavior in a transparent cylindrical convergent-divergent nozzle using a high-speed video camera. An effect of upstream pressure fluctuation due to a plunger pump is investigated from a viewpoint of unsteady behavior in a cavitating water jet. As a result, it is found that the cavitating flow has two kinds of oscillation patterns in the cavity length (cavitation cloud region). One is due to the upstream pressure fluctuation caused by the plunger pump. The other is much shorter periodic motion related to the characteristic oscillation of cavitation clouds accompanied with the shrinking (reentrant), growing and shedding motion of the clouds. 展开更多
关键词 cloud cavitation PERIODIC Behavior Water JET High-Speed Video OBSERVATION Image Analysis
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射流对绕水翼云空化流动抑制机理研究 被引量:8
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作者 王巍 张庆典 +3 位作者 唐滔 安昭阳 佟天浩 王晓放 《力学学报》 EI CSCD 北大核心 2020年第1期12-23,共12页
为理解绕水翼云空化流动的发展机理和探究水翼吸力面开孔射流的影响,采用密度修正的RNG k-ε湍流模型和Schnerr-Sauer空化模型对原始NACA66(mod)水翼和采用射流后的水翼的云空化非定常过程进行模拟和对比分析;采用在水翼吸力面近壁区设... 为理解绕水翼云空化流动的发展机理和探究水翼吸力面开孔射流的影响,采用密度修正的RNG k-ε湍流模型和Schnerr-Sauer空化模型对原始NACA66(mod)水翼和采用射流后的水翼的云空化非定常过程进行模拟和对比分析;采用在水翼吸力面近壁区设立监测线的方法对近壁区的流场进行监测,得到近壁区汽相体积分数、回射流速度、压力及压力梯度的时空分布云图;开展了云空化流场特性的涡动力学分析,进而分析水翼云空化的发生机理和射流抑制空化的抑制机理.结果表明:游离型空泡在下游溃灭时产生强烈的局部高压,其向上游传播导致前缘空穴的一次回缩,而空穴的二次回缩受回射流的影响.回射流的发展区域受限于较高的压力梯度,高的压力梯度一直存在,但回射流在一个周期内的首次出现需要时间的积累.在水翼吸力面射流使得射流孔附近压力升高,弥补了由于空化和绕流造成的压降,压力梯度增大,抗逆压能力增强,对回射流起到阻挡作用;另一方面,射流使得回射流区域面积和回射流的强度也有所减小,从而对云空化的发展起到抑制的效果.Q准则的涡结构云图相比于汽相体积分数云图能显示复杂的流动结构,前缘附着型空穴和尾缘游离型空穴内存在旋涡,回射流对空穴存在剪切作用造成空穴脱落.而射流对空穴和回射流的剪切和阻挡使云空化发展得到抑制. 展开更多
关键词 空化抑制 水翼 回射流 云空化 涡结构
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Bubbly shock propagation as a mechanism of shedding in separated cavitating flows 被引量:5
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作者 Harish Ganesh Simo A.Makiharju Steven L.Ceccio 《Journal of Hydrodynamics》 SCIE EI CSCD 2017年第6期907-916,共10页
Stable attached partial cavitation in separated flows can transition to cloud shedding, and the mechanism of transition has been attributed to the presence of a re-entrant liquid jet. Our findings have revealed the pr... Stable attached partial cavitation in separated flows can transition to cloud shedding, and the mechanism of transition has been attributed to the presence of a re-entrant liquid jet. Our findings have revealed the presence of propagating bubbly shock waves as an alternative dominant mechanism of shedding when the compressibility of the bubbly mixture is appreciable. In the present paper, we discuss dynamics associated with these bubbly shock waves, interaction of shock waves with obstacles in their path, and means to manipulate their properties to control the shedding process by non-condensable gas injection. 展开更多
关键词 Partial cavitation bubbly shock waves cloud cavitation X-ray densitometry
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The influence of surface roughness on cloud cavitation flow around hydrofoils 被引量:6
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作者 Jiafeng Hao Mindi Zhang Xu Huang 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2018年第1期10-21,共12页
The aim of this study is to investigate experimentally the effect of surface roughness on cloud cavitation around Clark-Y hydrofoils. High-speed video and particle image velocimetry(PIV) were used to obtain cavitation... The aim of this study is to investigate experimentally the effect of surface roughness on cloud cavitation around Clark-Y hydrofoils. High-speed video and particle image velocimetry(PIV) were used to obtain cavitation patterns images(Prog. Aerosp. Sci. 37: 551–581, 2001), as well as velocity and vorticity fields. Results are presented for cloud cavitating conditions around a Clark-Y hydrofoil fixed at angle of attack of α = 8? for moderate Reynolds number of Re = 5.6 × 10~5. The results show that roughness had a great influence on the pattern, velocity and vorticity distribution of cloud cavitation. For cavitating flow around a smooth hydrofoil(A) and a rough hydrofoil(B), cloud cavitation occurred in the form of finger-like cavities and attached subulate cavities, respectively. The period of cloud cavitation around hydrofoil A was shorter than for hydrofoil B.Surface roughness had a great influence on the process of cloud cavitation. The development of cloud cavitation around hydrofoil A consisted of two stages:(1) Attached cavities developed along the surface to the trailing edge;(2) A reentrant jet developed, resulting in shedding and collapse of cluster bubbles or vortex structure. Meanwhile, its development for hydrofoil B included three stages:(1) Attached cavities developed along the surface to the trailing edge, with accumulation and rotation of bubbles at the trailing edge of the hydrofoil affecting the flow field;(2) Development of a reentrant jet resulted in the first shedding of cavities. Interaction and movement of flows from the pressure side and suction side brought liquid water from the pressure side to the suction side of the hydrofoil, finally forming a reentrant jet. The jet kept moving along the surface to the leading edge of the hydrofoil, resulting in large-scale shedding of cloud bubbles. Several vortices appeared and dissipated during the process;(3) Cavities grew and shed again. 展开更多
关键词 Surface roughness EXPERIMENTS cloud cavitation Hydrofoils
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垂直发射条件下水下航行体通气云空泡的数值模拟与实验 被引量:2
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作者 任泽宇 王小刚 +1 位作者 程少华 权晓波 《航空学报》 EI CAS CSCD 北大核心 2023年第21期258-268,共11页
针对垂直发射条件下通气云空泡的流动特性,以水下航行体为研究对象,采用改进型延迟分离涡模型(IDDES)进行非定常数值模拟,通过引入混合尺度加速了雷诺时均(RANS)到大涡模拟(LES)的转换计算,提高了湍流应力的计算精度;同时搭建了垂直约... 针对垂直发射条件下通气云空泡的流动特性,以水下航行体为研究对象,采用改进型延迟分离涡模型(IDDES)进行非定常数值模拟,通过引入混合尺度加速了雷诺时均(RANS)到大涡模拟(LES)的转换计算,提高了湍流应力的计算精度;同时搭建了垂直约束式水下发射平台,采用定量排气的方式研究了通气云空泡的发展过程,验证了数值方法的有效性。研究发现:气液交界面在旋涡流动的作用下发生失稳,部分水相通过气液界面汇入通气空泡中发生气液掺混,形成云空泡;云空泡的发展为尺寸扩张和气液掺混同时进行的动态发展过程;在通气云空泡的作用下,流体速度梯度是云空泡影响涡量输运的主要作用因素。 展开更多
关键词 水下航行体 垂直发射 通气空泡 云空泡 涡量输运(IDDES)
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不同空泡脱落模式下空化多尺度特性研究
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作者 田北晨 李林敏 黄彪 《水动力学研究与进展(A辑)》 CSCD 北大核心 2024年第1期87-96,共10页
云状空化是一种以相变为核心,包含多种尺度空泡生长演变行为的强瞬态多相流动现象。该文采用双向耦合欧拉-拉格朗日多尺度空化模型,模拟了空化数σ=1.2时,绕8°攻角三维NACA66水翼空化流动,通过VOF(volume of fluid)界面捕捉法求解... 云状空化是一种以相变为核心,包含多种尺度空泡生长演变行为的强瞬态多相流动现象。该文采用双向耦合欧拉-拉格朗日多尺度空化模型,模拟了空化数σ=1.2时,绕8°攻角三维NACA66水翼空化流动,通过VOF(volume of fluid)界面捕捉法求解欧拉体系下大尺度空穴演化,利用拉格朗日体系下的离散空泡模型(DBM)追踪亚网格尺度离散空泡运动及生长溃灭过程。结果表明:绕水翼云状空化流动,包含附着型片状空泡生长与发展、回射流产生与推进、云状空泡脱落和宏观片空泡再次生长以及压力波推进4个阶段。离散空泡数量及尺度随大尺度空穴周期性演变而变化,主要分布在强湍流脉动区。在各空化发展阶段,离散空泡集中分布在水翼中后部,微空泡直径概率密度函数均符合单峰Gamma分布,最高空泡数密度泡径为50μm。在湍动程度较小的附着型空穴生长阶段,微空泡数密度相对于空泡直径呈-5/3幂率特征;在湍动程度较大的回射流发展阶段、云状空穴脱落溃灭及压力波推进阶段,较小尺度的微空泡数密度相对于空泡直径呈-2/3幂率特征,较大尺度的微空泡数密度相对于空泡直径呈-6幂率特征。 展开更多
关键词 云状空化 多尺度 欧拉-拉格朗日
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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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Effect of water injection on the cavitation control:experiments on a NACA66(MOD)hydrofoil 被引量:5
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作者 W.Wang T.Tang +4 位作者 Q.D.Zhang X.F.Wang Z.Y.An T.H.Tong Z.J.Li 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2020年第5期999-1017,I0001,共20页
The objective of this work is to investigate experimentally controlling cavitating flow over NACA66(MOD)hydrofoils by means of an active water injection along its suction surface.The continuous water vertically jets o... The objective of this work is to investigate experimentally controlling cavitating flow over NACA66(MOD)hydrofoils by means of an active water injection along its suction surface.The continuous water vertically jets out of the chamber inside the hydrofoil through evenly distributed surface holes.Experiments were carried out in cavitation water tunnel.using high-speed visualization technology and the particle image velocimetry(PIV)system to study the sheetlcloud cavity behaviors.We studied the effects of this active control on cavity evolution with four kinds of jet flow at two different jet positions.We analyzed the effect of water injection on the mechanism of the cavitating flow control.The results were all compared with that for the original hydrofoil without jet and show that the active jet can effectively suppress the sheet/cloud cavitation characterized by shrinking the attached cavity size and breaking the large-scaled cloud sheding vortex cavity into small-scaled ones.The optimum effectiveness of cavitation suppression is affected by the jet flow rates and jet positions.The water injection at flow rate coefficient 0.0245 with the jet position of 0.45C reduces the maximum sheet cavity length by 79.4%and the cavity shedding is diminished completely,which gives the most superior effect of sheet cavitation suppression.The jet blocks the re-entrant jet moving upstream and weakens the power of re-entrant jet and thus restrains the cavitation development effectively and stabilizes the flow field. 展开更多
关键词 cavitation active control Sheet/cloud cavitation.Water injection Re-entrant jet
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The Numerical Simulation of Collapse Pressure and Boundary of the Cavity Cloud in Venturi 被引量:6
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作者 张晓冬 付勇 +1 位作者 李志义 赵宗昌 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2009年第6期896-903,共8页
The idea that the collapse proceeds from the outer boundary of the cavity cloud towards its center for the ultrasonic cavitation proposed by Hasson and Morch in 1980s is further developed for calculating the collapse ... The idea that the collapse proceeds from the outer boundary of the cavity cloud towards its center for the ultrasonic cavitation proposed by Hasson and Morch in 1980s is further developed for calculating the collapse pressure and boundaries of cavity cloud at the collapse stage of bubbles for hydraulic cavitation flow in Venturi in present research. The numerical simulation is carried out based on Gilmore's eouations of bubble dynamics, which take account of the compressibility of fluid besides the viscosity and interfacial tension. The collapse of the cavity cloud is considered to proceed layer by layer from the outer cloud towards its inner part. The simulation results indicate that thepredicted boundaries of the cavity cloudat the collapse stage agree.well with the exPerimental ones.It is also found that the maximum collapse pressure of the cavity cloud is several times as high as the collapse pressure of outside boundary, and it is located at a point in the axis, where the cavity cloud disappears completely. This means that a cavity cloud has higher collapse pressure or strength than that of a single bubble due to the interactions of the bubbles. The effects of operation and structural parameters on the collapse pressure are also analyzed in detail. 展开更多
关键词 cavity cloud collapsing layer by layer laydrodynamic cavitation collapse pressure bubble dynamics
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微颗粒强化射流空化及破岩能力研究 被引量:1
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作者 楚恒智 郭勇 +4 位作者 张楠 刘斌 任铭 郝晨 毕文欣 《石油机械》 北大核心 2023年第8期34-42,共9页
深井、超深井钻井面临地层强度高、机械钻速慢等挑战,利用射流空化作用辅助破碎岩石为深井提速提供了新方向。为此,提出了利用微颗粒降低空化临界负压,提高空化强度的技术思路。采用高速摄影和水听器,证实了微颗粒对射流空化的强化作用... 深井、超深井钻井面临地层强度高、机械钻速慢等挑战,利用射流空化作用辅助破碎岩石为深井提速提供了新方向。为此,提出了利用微颗粒降低空化临界负压,提高空化强度的技术思路。采用高速摄影和水听器,证实了微颗粒对射流空化的强化作用,并通过冲蚀破岩试验探索了微颗粒直径、质量分数及喷距对空化射流破岩能力的影响规律。研究结果表明:微颗粒的存在可提供额外的空化核,同时降低了空化初生难度,可提高井底射流的空化强度;随着微颗粒质量分数的增加,空泡云趋于稳定,空化的周期性特征逐渐消失,微颗粒的磨蚀作用和空泡的冲蚀作用将在岩石表面共同形成辅助破岩效果;随着喷距增大,空化破坏作用先增加后减小,无因次喷距为100时空化射流冲蚀效果最佳;优化设计钻头水眼到井底岩石的距离,是保障空化射流辅助破岩效果的关键。研究结果可为提高深部难钻地层射流辅助破岩效率提供参考。 展开更多
关键词 深井钻井 空化射流 空泡云 高速摄影 空化噪声 破岩
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Large eddy simulation of cloud cavitation and wake vortex cavitation around a trailing-truncated hydrofoil 被引量:4
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作者 Ting-yun Yin Giorgio Pavesi +2 位作者 Ji Pei Shou-qi Yuan Xing-cheng Gan 《Journal of Hydrodynamics》 SCIE EI CSCD 2022年第5期893-903,共11页
The cavitation has received considerable attention for decades because of its negative influence on the performance and the safety of the hydraulic machinery.In this study,a large eddy simulation is carried out to num... The cavitation has received considerable attention for decades because of its negative influence on the performance and the safety of the hydraulic machinery.In this study,a large eddy simulation is carried out to numerically investigate the unsteady cavitating flow around a trailing-truncated NACA 0009 hydrofoil for determining the underlying physical mechanisms.Two types of cavitation morphologies are identified:The large-scale bubble cluster and the von Kármán vortex cavity,named as the cloud cavitation and the wake vortex cavitation,respectively.It is shown that the velocity profiles obtained over the hydrofoil suction surface are in good agreement with the experimental data,indicating the accuracy of the current simulation.The dynamic evolution of the sheet/cloud cavity is also well reproduced,covering the sheet cavity breakup,the sheet/cloud transformation,and the collapse of the cloudy bubble cluster.The wake-vortex cavitation is caused by the blunt geometry at the hydrofoil trailing edge,where pairs of vortex cavities are induced.Both the cloud and vortex cavities significantly affect the lift oscillation,which makes it difficult to decompose the components.The fundamental shedding mechanisms of the wake vortex cavitation are discussed based on the finite-time Lyapunov exponent field.Specifically,the suction-side bubble grows and squeezes the giant pressure bubble away from the trailing edge.After the pressure bubble detaches,a new counterclockwise vortex or a new bubble appears at the pressure side,thus lifting the ridge towards the suction trailing edge and generating a strong vortex eye that pinches off the trailing portion of the suction-side bubble. 展开更多
关键词 cloud cavitation wake vortex cavitation trailing-truncated hydrofoil large eddy simulation
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