Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination
Author:
Affiliation:
1. Technische Universität Berlin, Germany
Funder
Bundesministerium für Wirtschaft und Energie
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060594
Reference49 articles.
1. Comprehensive Thermodynamic Analysis of the Humphrey Cycle for Gas Turbines with Pressure Gain Combustion
2. There's a New Cycle in Town
3. Recent Developments in the Research on Pressure-Gain Combustion Devices
4. Potential Benefits to Commercial Propulsion Systems from Pressure Gain Combustion
Cited by 35 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. Analysis of coupling supersonic turbine stage with rotating detonation combustor under different turbine parameters;Aerospace Science and Technology;2024-10
2. Experimental study on upstream pressure characteristics of rotating detonation engine with methane and oxygen-enriched air;Aerospace Science and Technology;2024-10
3. Numerical investigation of sweeping jet actuator on oblique detonation;Combustion and Flame;2024-10
4. Performance and Exergy analysis of TurboJet and TurboFan configurations with Rotating Detonation Combustor;International Journal of Thermofluids;2024-08
5. Numerical Investigation on the Influence of Continuous Rotating Backpropagation Pressure Wave on Turbine Performance;Journal of Engineering for Gas Turbines and Power;2024-07-16
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