首页 | 本学科首页   官方微博 | 高级检索  
     

不同湍流模型在旋流非接触搬运器仿真中的应用和对比
引用本文:蒲汲君, 熊鹰. 三维水翼梢涡流场数值研究[J]. 中国舰船研究, 2017, 12(1): 8-13, 26. DOI: 10.3969/j.issn.1673-3185.2017.01.002
作者姓名:蒲汲君  熊鹰
作者单位:海军工程大学 舰船工程系, 湖北 武汉 430033
基金项目:国家自然科学基金资助项目(51179198)
摘    要:
针对三维水翼梢涡流场和梢涡空泡初生的问题,分别建立k-ω,DES和LES模型,对水翼的梢涡流场进行计算研究。为减少误差,在网格的处理上对梢涡流域进行局部加密,对未发生空化时梢涡内的轴向速度和切向速度进行计算,发现LES模型的计算结果与实验值吻合较好。
在此基础上,讨论尾涡的卷曲对梢涡压力场的影响,提出了使用气泡静力平衡方程计算初始梢涡空泡数的方法。


关 键 词:梢涡  气泡静力平衡方程  空泡初生  水翼
收稿时间:2016-06-03

Some observations of tip-vortex cavitation
PU Jijun, XIONG Ying. Numerical study of hydrofoil tip vortex fluid field[J]. Chinese Journal of Ship Research, 2017, 12(1): 8-13, 26. DOI: 10.3969/j.issn.1673-3185.2017.01.002
Authors:PU Jijun  XIONG Ying
Affiliation:Department of Naval Architecture Engineering, Naval University of Engineering, Wuhan 430033, China
Abstract:
Three different models, k-ω, DES and LES, are conducted in the analysis of the tip vortex flow field. In order to reduce the discrete error induced by the grid, mesh refinement is applied to the area of the tip vortex core in numerical simulations.
The axis and tangential velocities of the tip vortex flow field with no cavitation are calculated, and the calculated velocities agree well with the experimental results. On the basis of this process, the influence of vortex roll-up on the tip vortex pressure filed is discussed, and bubble static equilibrium is proposed by which the tip vortex cavitation inception number is computed.
Keywords:tip vortex  bubble static equilibrium  cavitation inception  hydrofoil
点击此处可从《中国舰船研究》浏览原始摘要信息
点击此处可从《中国舰船研究》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号