Effect of Throttling on Dual-Bell Sneak-Transition Side Loads
Author:
Affiliation:
1. Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India
2. Technical University of Munich, 85748 Garching, Germany
Funder
Alexander von Humboldt-Stiftung
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38095
Reference29 articles.
1. Critical Assessment of Dual-Bell Nozzles
2. FosterC.CowlesF. “Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors,” ORDCIT Project, Progress Rept. 4-103, Jet Propulsion Lab., California Inst. of Technology, Pasadena, CA, 1949.
3. SuttonN. N. “Liquid Rocket Engine Nozzles,” NASA Space Vehicle Design Criteria, NASA SP-8120, 1976.
4. Advanced Rocket Nozzles
5. An Analytical Study on Design and Performance of Dual-Bell Nozzles
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