船舶 ›› 2020, Vol. 31 ›› Issue (03): 89-94.DOI: 10.19423/j.cnki.31-1561/u.2020.03.089

• 船型推介 • 上一篇    下一篇

基于RANS方法的NACA0009水翼梢隙涡数值模拟

万初瑞1,2, 严鹏1,2, 王建强2   

  1. 1.喷水推进技术重点实验室 上海200011;
    2.中国船舶及海洋工程设计研究院 上海200011
  • 收稿日期:2019-09-23 修回日期:2019-10-23 出版日期:2020-06-25 发布日期:2021-08-20
  • 作者简介:万初瑞(1985-),男,博士,高级工程师。研究方向:船舶推进。严 鹏(1990-),男,博士,工程师。研究方向:船舶及海洋工程、CFD分析。王建强(1990-),男,博士,工程师。研究方向:船舶推进。

Numerical Simulation of Tip Clearance Vortex of NACA0009 Hydrofoil Based on RANS Method

WAN Chu-rui1,2, YAN Peng1,2, WANG Jian-qiang2   

  1. 1. State Key Laboratory of Water-jet Propulsion, Shanghai 200011,China;
    2. Marine Design & Research Institute of China, Shanghai 200011, China
  • Received:2019-09-23 Revised:2019-10-23 Online:2020-06-25 Published:2021-08-20

摘要: 梢隙涡空泡计算是一项具有挑战的课题。文章以准确预报水翼和壁面之间的梢隙涡为目的,采用雷诺平均应力(RANS)结合Schnerr和Sauer模型方法进行数值研究。对于无空泡状态,不同湍流模式的适用性研究结果表明SST 模型具备较高精度;对于有空泡状态,研究结果发现空泡的存在使涡心轨迹发生一定改变,使其更加贴近壁面和吸力面。通过研究分析得到诱导空蚀发生的一个重要因素,且表明梢隙涡空泡观测预报梢隙涡具有一定应用价值。

关键词: 梢隙涡, 湍流模型, 涡轨迹, 空泡

Abstract: The simulation of the tip clearance vortex cavitation is a challenging project due to the difficulty of defining the mass source item. The numerical simulation is conducted by using the Reynolds-averaged Navier-stokes (RANS) method with the Schnerr and Sauer cavitation model, in order to accurately predict the tip clearance vortex between the hydrofoil and the wall. For no cavitating flows, the results with the different turbulence models show the high accuracy of the SST k-ω model. For cavitating flows, the results show that the cavitation will change the trajectory of the vortex core, making it closer to the wall and the suction side. The current study shows that the tip clearance vortex can be predicted by the observation of the tip clearance vortex cavitation which may be one of the important factors inducing cavitation erosion.

Key words: Tip clearance vortex, turbulence model, vortex trajectory, cavitation

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