High Throughflow StreamVane Swirl Distortion Generators: Design and Analysis

Author:

Hayden Andrew P.1,Gillespie John2,Hefner Cole3,Untaroiu Alexandrina1,Lowe K. Todd2

Affiliation:

1. Department of Mechanical Engineering, Virginia Tech , Blacksburg, VA 24060

2. Department of Aerospace and Ocean Engineering, Virginia Tech , Blacksburg, VA 24060

3. Techsburg, Inc. , 265 Industrial Dr. NE, Christiansburg, VA 24073

Abstract

Abstract In recent years, the StreamVane technology has developed into a mature and streamlined process that can reproduce swirl distortion for ground-test evaluation of fan and compressor performance and durability. A StreamVane device consists of complex turning vanes that accurately output a distorted secondary velocity field at a defined distance downstream. To further advance the applications and conditions in which these devices operate, a research effort was developed and completed to investigate methods to increase critical Mach numbers. The effort was split into three separate stages: (1) Perform high fidelity computational fluid dynamics (CFD) to identify peak Mach number locations within twin and quad swirl vane pack designs; (2) conduct thorough literature reviews on relevant high throughflow techniques; and (3) design and implement selected techniques to evaluate improvements using the same high-fidelity CFD methods. It was predicted that employing blade lean within high-speed vane junctions increased critical Mach numbers by 6.6%, while blade sweep resulted in a 3.5% increase. The results and conclusions from this effort are presented throughout this paper with a primary focus on comparing Mach numbers and swirl profiles between vane packs with and without high throughflow designs.

Funder

Air Force Research Laboratory

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference45 articles.

1. The Stream-Vane Method: A New Way to Generate Swirl Distortion for Jet Engine Research,2013

2. Compressor Performance and Operability in Swirl Distortion;ASME J. Turbomach.,2012

3. Stereoscopic PIV Measurements of Swirl Distortion on a Full-Scale Turbofan Engine Inlet,2014

4. Stereoscopic PIV Measurements in a Turbofan Engine Inlet With Tailored Swirl Distortion,2015

5. Fan Response to Inlet Swirl Distortions Produced by Boundary Layer Ingesting Aircraft Configurations,2015

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