Effects of pulsating backpressure on performance of stability of a centrifugal compressor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference27 articles.
1. Large eddy simulations of spray combustion instability in an aero-engine combustor at elevated temperature and pressure;Cheng;Aerosp. Sci. Technol.,2021
2. Rotating detonation engine operation;Suchocki,2012
3. Detonative propulsion;Wolański;Proc. Combust. Inst.,2013
4. Influence of altitude on two-stage turbocharging system in a heavy-duty diesel engine based on analysis of available flow energy;Yang;Appl. Therm. Eng.,2018
5. An experimental investigation of the non-steady flow characteristics of a centrifugal compressor;Benson;Proc. Inst. Mech. Eng.,1965
Cited by 4 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. Numerical research on performance of new structure centrifugal compressor for supercritical CO2 power systems;Annals of Nuclear Energy;2024-05
2. Spatiotemporal characteristics of rotating stall in a centrifugal compressor with a volute at low-flow rate conditions;Physics of Fluids;2024-03-01
3. Research on the performance characteristics of hydrogen circulation pumps for PEMFC vehicles;International Journal of Hydrogen Energy;2024-01
4. Dynamic mode characteristics of flow instabilities in a centrifugal compressor impeller;Aerospace Science and Technology;2023-11
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