Experimental investigations on pulse detonation rocket engine with various injectors and nozzles
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference21 articles.
1. Review of propulsion applications of detonation waves;Kailasanath;American Institute of Aeronautics and Astronautics Journal,2000
2. K. Kailasanath, A Review of PDE Research-Performance Estimates, AIAA Paper 2001-0474, 2001.
3. Performance validation of a single-tube pulse detonation rocket system;Kasahara;Journal of Propulsion and Power,2009
4. Pulse detonation propulsion: challenges, current status, and future perspective;Roy;Progress in Energy and Combustion Science.,2004
5. Deflagration to detonation transition processes by turbulence-generating obstacles in pulse detonation engines;Lee;Journal of Propulsion and Power,2004
Cited by 22 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. Investigation of Spray Characteristics for Detonability: A Study on Liquid Fuel Injector and Nozzle Design;Aerospace;2024-05-23
2. Effect of incoming flow on the detonation re-initiation in liquid n-heptane/air mixtures;Acta Astronautica;2024-05
3. Investigation on the effect of injector modification on injector atomization and U-bend pulse detonation combustion characteristics;Thermal Science;2023
4. Numerical simulation of detonation re-initiation in a 90° bifurcated channel filled with n-heptane/air mixture;Acta Astronautica;2023-01
5. Performance analysis of a hybrid pulse detonation engine using liquid hydrogen as fuel;International Journal of Hydrogen Energy;2022-06
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