Investigation of Film Cooling Effectiveness of Dual-fanned Hole with Various Exit Widths

Author:

Guang-Chao Li1,Shuai Zhou1,Wei Zhang1,Zhi-hai Kou1,Rang-shu Xu1

Affiliation:

1. Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang110136, China

Abstract

AbstractFilm cooling effectiveness downstream of one row of holes of 30 degree inclination angle was measured by using a steady-state thermochromic liquid crystal technique at blowing ratios of 0.5, 1.0, 1.5 and 2.0, respectively. Three kinds of dual-fanned holes which have the same expanded entrance width and the different expanded exit widths were tested. The configuration of only expanded entrance, but cylindrical exit hole, was tested to examine the effect of the expanded entrance on film cooling performance. The numerical simulation for the three expanded exit configurations was carried out explaining the mechanism of film cooling by the flow and thermal field. The only expanded entrance has a weak influence on film cooling effectiveness. The ${W_o} = 1.5d$ configuration provides a lift of film cooling effectiveness compared to ${W_o} = 1.0d$ configuration. Film cooling effectiveness is not sensitive to the change of configurations from ${W_o} = 1.5d$ to ${W_o} = 2.0d$. Film cooling effectiveness for ${W_o} = 2.5d$ performs significantly better than the other configurations due to the presence of the anti-vortex. The effect of dual-fanned exit width on film cooling effectiveness is strongly dependent on the blowing ratios.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Reference42 articles.

1. Film cooling performance of converging-slot holes with different exit-entry area ratios[J];ASME J Turbomach,2011

2. Film-cooling performance of antivortex hole on a flat plate[J];ASME J Turbomach,2013

3. Effect of a crossflow at the entrance to a film-cooling hole[J];ASME J Fluids Eng,1997

4. Film cooling effectiveness due to discrete holes within a transverse surface slot[R];ASME Paper,2002

5. Effects of hole geometry and density on three-dimensional film cooling[J];J Heat Mass Transfer,1974

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