Sub Scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Loads(II)-Influence of a Step in Nozzle Contour on Side-Load
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference4 articles.
1. Restricted Shock Separation in Rocket Nozzles
2. Watanabe, Y. "LE-7A Engine Nozzle Separation Phenomenon During the Transient Process," ISTS 2002-a-24, 2002
3. Tomita, T. et al. "Sub-scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Loads(I)-Formation of RSS Structure Due to Combustion Condition," AIAA 2002-3842, 2002
4. Takahashi, M. et al. "Transient Flow Simulation of a Compressed Truncated Perfect Nozzle," AIAA 2001-3681, 2001
Cited by 6 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. Experimental evaluation of side-loads in LE-7A prototype engine nozzle;Shock Waves;2009-03-26
2. Next Booster Engine LE-X in Japan;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
3. Stagnation and Jump Phenomenon of Separation Point by Step inside LE-7A Engine Nozzle;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
4. Strong Side-Load Observed on a Parabolic Nozzle with No RSS Flow Pattern;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10
5. LE-7A Engine Nozzle Flow Separation Phenomenon and the Possibility of RSS Suppression by the Step Inside the Nozzle;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
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