Experimental measurement of tip vortex flow field with/without cavitation in an elliptic hydrofoil

IF 3.4 3区 工程技术 Q1 MECHANICS
Xiao-xing Peng (彭晓星), Liang-hao Xu (徐良浩), Yu-wen Liu (刘玉文), Guo-ping Zhang (张国平), Yan-tao Cao (曹彦涛), Fang-wen Hong (洪方文), Kai Yan (颜开)
{"title":"Experimental measurement of tip vortex flow field with/without cavitation in an elliptic hydrofoil","authors":"Xiao-xing Peng (彭晓星),&nbsp;Liang-hao Xu (徐良浩),&nbsp;Yu-wen Liu (刘玉文),&nbsp;Guo-ping Zhang (张国平),&nbsp;Yan-tao Cao (曹彦涛),&nbsp;Fang-wen Hong (洪方文),&nbsp;Kai Yan (颜开)","doi":"10.1016/S1001-6058(16)60808-9","DOIUrl":null,"url":null,"abstract":"<div><p>In this paper, recent measurements of tip vortex flow with and without cavitation carried out in Cavitation Mechanism Tunnel of China Ship Scientific Research Center (CSSRC) are presented. The elliptic hydrofoil with section NACA 66<sub>2</sub>-415 was adopted as test model. High-speed video (HSV) camera was used to visualize the trajectory of tip vortex core and the form of tip vortex cavitation (TVC) in different cavitation situations. Laser Doppler velocimetry (LDV) was employed to measure the tip vortex flow field in some typical sections along the vortex trajectory with the case of cavitation free. Stereo particle image velocimetry (SPIV) system was used to measure the velocity and vorticity distributions with and without cavitation. Series measurement results such as velocity and vorticity distributions, the trajectory of tip vortex core, the vortex core radius, cavity size and cavitation inception number were obtained. The results demonstrated that the minimum pressure coefficient in the vortex core obtained by flow field measurement was quite coincident with the tip vortex cavitation inception number obtained under the condition of high incoming velocity and low air content. And TVC would decrease the vortex strength comparing with the case without cavitation.</p></div>","PeriodicalId":66131,"journal":{"name":"水动力学研究与进展:英文版","volume":"29 6","pages":"Pages 939-953"},"PeriodicalIF":3.4000,"publicationDate":"2017-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1001-6058(16)60808-9","citationCount":"31","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"水动力学研究与进展:英文版","FirstCategoryId":"1087","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1001605816608089","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 31

Abstract

In this paper, recent measurements of tip vortex flow with and without cavitation carried out in Cavitation Mechanism Tunnel of China Ship Scientific Research Center (CSSRC) are presented. The elliptic hydrofoil with section NACA 662-415 was adopted as test model. High-speed video (HSV) camera was used to visualize the trajectory of tip vortex core and the form of tip vortex cavitation (TVC) in different cavitation situations. Laser Doppler velocimetry (LDV) was employed to measure the tip vortex flow field in some typical sections along the vortex trajectory with the case of cavitation free. Stereo particle image velocimetry (SPIV) system was used to measure the velocity and vorticity distributions with and without cavitation. Series measurement results such as velocity and vorticity distributions, the trajectory of tip vortex core, the vortex core radius, cavity size and cavitation inception number were obtained. The results demonstrated that the minimum pressure coefficient in the vortex core obtained by flow field measurement was quite coincident with the tip vortex cavitation inception number obtained under the condition of high incoming velocity and low air content. And TVC would decrease the vortex strength comparing with the case without cavitation.

椭圆型水翼有/无空化时叶顶涡流场的实验测量
本文介绍了近年来在中国船舶科学研究中心空化机理隧道中进行的有空化和无空化叶尖涡流动的测量结果。以截面为NACA 662-415的椭圆型水翼为试验模型。采用高速视频(HSV)摄像机对不同空化情况下叶顶涡核的运动轨迹和叶顶涡空化的形态进行了可视化研究。采用激光多普勒测速仪(LDV)对无空化情况下沿涡轨迹的典型截面的叶顶涡流场进行了测量。采用立体粒子图像测速系统(SPIV)测量了有空化和无空化条件下的速度和涡度分布。得到了速度和涡度分布、叶顶涡核轨迹、涡核半径、空腔尺寸和空化起始数等一系列测量结果。结果表明:流场测量得到的涡核最小压力系数与高速度低空气含量条件下得到的尖涡空化起始数基本吻合;与无空化情况相比,TVC会降低涡强度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
CiteScore
5.90
自引率
0.00%
发文量
1240
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信