Effects of Boundary Layer Control Method on Hydrodynamic Characteristics and Tip Vortex Creation of a Hydrofoil

Author:

Ghadimi Parviz1,Tanha Araz2,Kourabbasloo Navid Nemati3,Tavakoli Sasan4

Affiliation:

1. Amirkabir University of Technology, Tehran , Islamic Republic of Iran

2. Amirkabir University of Technology Tehran , Islamic Republic of Iran

3. Sharif University of Technology, Tehran , Islamic Republic of Iran

4. Amirkabir University of Technology, 424 Hafez Ave., 03314 Tehran , Islamic Republic of Iran

Abstract

Abstract There is currently a significant focus on using boundary layer control (BLC) approach for controlling the flow around bodies, especially the foil sections. In marine engineering this is done with the hope of increasing the lift - to - drag ratio and efficiency of the hydrofoils. In this paper, effects of the method on hydrodynamic characteristics and tip vortex formation of a hydrofoil are studied. Steady water injection at the tip of the hydrofoil is simulated in different conditions by using ANSYS-CFX commercial software. Validity of the proposed simulations is verified by comparing the obtained results against available experimental data. Effects of the injection on the lift, drag, and lift - to - drag ratio are studied and the ranges within which the injection has the most positive or negative effects, are determined. Furthermore, flow pattern and pressure variation are studied upon the water injection to determine the most positive and negative case and to ascertain the main reasons triggering these phenomena.

Publisher

Walter de Gruyter GmbH

Subject

Mechanical Engineering,Ocean Engineering

Reference34 articles.

1. 1. Kroo, I. : Non-planar wings concepts for increases aircraft efficiency. VKI lecture series on Innovative Configurations and Advanced Concepts for Future Civil Aircraft, 2005.

2. 2. Park, K., Lee J. Influence of endplate on aerodynamic characteristics of low-aspect ratio wing in ground effect. J. Mech. Sci. Tech., 22, 2578-2589, 2008.

3. 3. Kaplan S.M., Altman A. : Wake Vortices Measurements for Low Aspect Ratio Wings at Low Reynolds Number. J. Aircraft. 44, 1631-1639, 2007.

4. 4. Mansour, N.N. : Numerical Simulation of the Tip Vortex of a Low Aspect Ratio Wing at Transonic Speed. AIAA, 23, 1143-1149, 1985.

5. 5. McAlister, K.W., Takashi T.K. : NACA 0015 Wing Pressure and Trailing Vortex Measurements. ACSOM Technical Report 91-A-003, California, 1991.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3