The Effect of Reynolds Number and Turbulence Intensity on the Performance of a Compressor Cascade with Prescribed Velocity Distribution
Author:
Affiliation:
1. Research Engineer, National Institute for Machine Design, Bechovice, Czechoslovakia
2. Department of Mechanical Engineering, The University of Liverpool. Fellow of the Institution
Abstract
Publisher
SAGE Publications
Subject
General Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1243/JMES_JOUR_1977_019_022_02
Reference5 articles.
1. Approximate Calculation of the Laminar Boundary Layer
Cited by 9 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
1. Effects of the Reynolds Number on the Efficiency and Stall Mechanisms in a Three-stage Axial Compressor;Journal of Applied Fluid Mechanics;2024-06-01
2. Numerical Investigation of Low Reynolds Number Effects on Energy Loss inside Centrifugal Compressor with Different Inlet Conditions;Aerospace Science and Technology;2024-03
3. Control of shock–boundary layer interaction in a transonic compressor cascade via heat transfer at a low Reynolds number;Applied Thermal Engineering;2024-02
4. Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles;Chinese Journal of Aeronautics;2022-03
5. Effects of Reynolds number and loading distribution on the aerodynamic performance of a high subsonic compressor airfoil;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2020-01-13
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