Swirl Effects on Spinning Solid Propellant Rocket Motor Performance
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference16 articles.
1. Spin acceleration effects on some full-scale rocket motors.
2. Effects of acceleration upon solid-rocket performance.
3. An investigation of the acceleration induced burning rate increase of nonmetallized composite propellants
4. A photographic and analytic study of composite propellant combustionin an acceleration field
Cited by 5 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 high-speed spin on the reacting flow of drag reduction equipment under rapid depressurization;Applied Thermal Engineering;2022-02
2. Characteristics of the Reacting Flow for the Base‐Bleed Projectile under Dual Stress;Propellants, Explosives, Pyrotechnics;2021-10-28
3. Mechanism of Influence of High‐Speed Self‐Spin on Ignition Transients for a Solid Rocket Motor: a Numerical Simulation;Propellants, Explosives, Pyrotechnics;2020-04-20
4. Regression rate response in spin-stabilized solid fuel ramjets;Journal of Mechanics;2020
5. Clustering Analysis on Internal Flow Field of a Spinning Solid Rocket Motor Nozzle;2017 9th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC);2017-08
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