Study on the influence of surface microstructure of hydrofoil on cavitation characteristics

IF 6.4 2区 工程技术 Q1 MECHANICS
Ye Cai , Yunqing Gu , Yun Ren , Longbiao Ma , Chengqi Mou , Qianfeng Qiu , Denghao Wu , Zhenxing Wu , Jiegang Mou
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引用次数: 0

Abstract

In order to better suppress the occurrence of cavitation, a hydrofoil model based on microjet structure and micro-wedge structure was established. The modified turbulence model shear stress transport (SST) k-ω is used to simulate the hydrofoil. By analyzing the vorticity distribution, flow field streamline, cavitation morphology, vortex structure and velocity vector distribution, the difference between the control effects of two kinds of airfoil surface microstructure on cavitation flow is studied, and the mechanism of micro wedge structure and micro jet structure on cavitation flow on airfoil surface is revealed. The results show that both microstructures show the suppression of vorticity distribution. The micro-wedge structure suppresses cavitation by affecting the turbulent kinetic energy of the near wall, the streamline vortex of the far wall and the vortex structure, accelerates the shedding and collapse of cavitation, and reduces the distribution of the low pressure region. When the chordwise position is 3.5 mm, the cavitation suppression effect is the most obvious. The microjet structure can affect the vortex motion on the far wall and hinder the upward development of the re-entrant jet. The larger the tangential jet ratio is, the stronger the jet intensity is. When the tangential jet ratio is 0.3 and 0.4, the suppression effect of the vortex motion is significant, the length of the low pressure distribution is smaller, and the shedding cavitation is accelerated from large scale to small scale.
水翼表面微观结构对空化特性影响的研究
为了更好地抑制空化现象的发生,建立了基于微射流结构和微楔结构的水翼模型。采用改进的湍流模型剪切应力输运(SST) k-ω来模拟水翼。通过对涡量分布、流场流线、空化形态、涡结构和速度矢量分布的分析,研究了两种翼型表面微结构对空化流动控制效果的差异,揭示了微楔结构和微射流结构对翼型表面空化流动的作用机理。结果表明,两种微观结构均表现出涡度分布的抑制。微楔结构通过影响近壁湍流动能、远壁流线涡和涡结构来抑制空化,加速空化的脱落和崩塌,减少低压区分布。弦向位置为3.5 mm时,空化抑制效果最明显。微射流结构会影响远壁面涡的运动,阻碍再入射流的向上发展。切向射流比越大,射流强度越强。切向射流比为0.3和0.4时,涡动抑制效果显著,低压分布长度较小,脱落空化由大尺度向小尺度加速;
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
11.00
自引率
10.00%
发文量
648
审稿时长
32 days
期刊介绍: International Communications in Heat and Mass Transfer serves as a world forum for the rapid dissemination of new ideas, new measurement techniques, preliminary findings of ongoing investigations, discussions, and criticisms in the field of heat and mass transfer. Two types of manuscript will be considered for publication: communications (short reports of new work or discussions of work which has already been published) and summaries (abstracts of reports, theses or manuscripts which are too long for publication in full). Together with its companion publication, International Journal of Heat and Mass Transfer, with which it shares the same Board of Editors, this journal is read by research workers and engineers throughout the world.
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