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Numerical analysis of a ventilated supercavity under periodic motion of the cavitator 被引量:2
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作者 Yun-hua Jiang Zhi-hui Zou +2 位作者 Jia Li Yao Yao Le-le Yang 《Journal of Hydrodynamics》 SCIE EI CSCD 2021年第6期1216-1229,共14页
This paper presents a numerical simulation of the geometry and the pressure distribution of a ventilated supercavity at different cavitator amplitudes and periods of motion.The numerical method is validated by compari... This paper presents a numerical simulation of the geometry and the pressure distribution of a ventilated supercavity at different cavitator amplitudes and periods of motion.The numerical method is validated by comparing with the results of a semi-empirical formula under specific conditions.It is shown that the simulation can capture the boundary fluctuations of the ventilated supercavity and its internal pressure variations in a cavitator motion cycle.The simulation results show that the supercavity boundary experiences wave-like deformations when the wavelength of the disturbance caused by the cavitator motion is comparable to the supercavity length.It is also shown that the supercavity closure changes in form between a re-entrant jet and a twin vortex owing to the variations of the pressure difference between the outside and the inside of the supercavity near the closure region.The maximum diameter of the ventilated supercavity exhibits periodic changes with a double peak in each cavitator motion cycle,caused by the corresponding changes of the difference between the internal and external pressures.With the increase of the amplitude of motion of the cavitator,the supercavity boundary has enhanced wave-like undulations,with an increased maximum diameter,and with fluctuations in the cavitation number.As the period of the cavitator motion increases,the wavelength of the disturbances caused by this motion becomes greater than the supercavity length,and so the wave-like undulations of the supercavity boundary and the maximum diameter of the supercavity gradually decrease,but the variations of the cavitation number increase.Moreover,with the increase of the periods,the delay effects on the variations of the characteristics of the supercavity geometry caused by cavitator motion gradually decrease,and they practically vanish for large periods. 展开更多
关键词 ventilated supercavity geometrical and pressure characteristics cavitator motion
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周期性阵风流对通气超空泡尾流结构影响的数值研究 被引量:1
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作者 王威 张志刚 +1 位作者 何广华 莫惟杰 《Journal of Marine Science and Application》 CSCD 2021年第1期34-45,共12页
A computational model is established to investigate the effects of a periodic gust flow on the wake structure of ventilated supercavities.The effectiveness of the computational model is validated by comparing with ava... A computational model is established to investigate the effects of a periodic gust flow on the wake structure of ventilated supercavities.The effectiveness of the computational model is validated by comparing with available experimental data.Benefited from this numerical model,the vertical velocity characteristics in the entire flow field can be easily monitored and analyzed under the action of a gust generator;further,the unsteady evolution of the flow parameters of the closed region of the supercavity can be captured in any location.To avoid the adverse effects of mounting struts in the experiments and to obtain more realistic results,the wake structure of a ventilated supercavity without mounting struts is investigated.Unsteady changes in the wake morphology and vorticity distribution pattern of the ventilated supercavity are determined.The results demonstrate that the periodic swing of the gust generator can generate a gust flow and,therefore,generate a periodic variation of the ventilated cavitation numberσ.At the peakσ,a re-entrant jet closure appears in the wake of the ventilated supercavity.At the valleyσ,a twin-vortex closure appears in the wake of the ventilated supercavity.For the forward facing model,the twin vortex appears as a pair of centrally rolled-up vortices,due to the closure of vortex is affected by the structure.For the backward facing model,however,the twin vortex appears alternately as a pair of centrally rolled-up vortices and a pair of centrally rolled-down vortices,against the periodic gust flow. 展开更多
关键词 ventilated supercavities Periodic gust flow Wake structure Vorticity distribution pattern Vortex structures
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THE COMPARATIVE STUDY OF VENTILATED SUPER CAVITY SHAPE IN WATER TUNNEL AND INFINITE FLOW FIELD 被引量:12
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作者 ZHOU Jing-jun YU Kai-ping MIN Jing-xin YANG Ming 《Journal of Hydrodynamics》 SCIE EI CSCD 2010年第5期689-696,共8页
In order to understand the difference of ventilated supercavity in water tunnel and infinite flow field, 3-D numerical simulations are carried out to obtain the ventilated supercavity in above mentioned conditions bas... In order to understand the difference of ventilated supercavity in water tunnel and infinite flow field, 3-D numerical simulations are carried out to obtain the ventilated supercavity in above mentioned conditions based on RANS equations, using the finite volume method and SST turbulence model in the framework of the two fluid multiphase flow model. The numerical method adopted in this article for the infinite flow field and water tunnel experiments is validated by comparing results with those of empirical formulas and experimental data. On this basis the difference between water tunnel experiments and infinite flow field is studied, including the influence of the route loss and the blocking effect in the water tunnel. Finally, some suggestions are made for water tunnel experiments. 展开更多
关键词 ventilated supercavity two fluid multiphase model ambient pressure viscous effect blocking effect cavitation number
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尾部射流作用下通气超空泡的瞬态动力学分析
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作者 向敏 周后村 +1 位作者 赵小宇 刘波 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第4期91-103,I0002,共14页
通气空化可应用于水下航行器以实现高减阻率.在推进系统产生的高速尾喷流的影响下,通气超空泡可能会发生变形、波动和不稳定,本文重点针对尾射流作用下通气超空泡瞬态演化动力学机制开展研究,实验在具有高除气率的开放式水洞系统中进行... 通气空化可应用于水下航行器以实现高减阻率.在推进系统产生的高速尾喷流的影响下,通气超空泡可能会发生变形、波动和不稳定,本文重点针对尾射流作用下通气超空泡瞬态演化动力学机制开展研究,实验在具有高除气率的开放式水洞系统中进行,详细记录了不同尾射流流量下气液界面的演变过程.采用可压缩多相流模型,结合剪切应力湍流模型和界面追踪方法,对流场进行了深入研究.随着射流速度从亚音速增加到声速,流场呈现三种不同的模式,分别为透明空泡(TC)、透明空泡-射流(TCJ)和变形空泡-射流(DC-J)模式.在TC模式下观察到-.种新的泄气机制,该机制下双涡管泄气与界面震荡泄气耦合.进一步对内部流场结构变化和局部压力脉动规律进行了详细讨论,得到流型随无量纲射流动量比和动能比的变化规律,所得结果可为通气超空泡的控制提供有价值的见解. 展开更多
关键词 ventilated supercavity Jet flow Gas-liquid flow Drag reduction
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