Numerical simulation of sloshing in the propellant tank of reusable rocket vehicle using meshfree method
Author:
Publisher
Springer Science and Business Media LLC
Subject
Computational Mathematics,Fluid Flow and Transfer Processes,Modeling and Simulation,Numerical Analysis,Civil and Structural Engineering,Computational Mechanics
Link
https://link.springer.com/content/pdf/10.1007/s40571-022-00488-4.pdf
Reference46 articles.
1. Mao Q, Dou LQ, Qun Z, Ding ZT (2018) Attitude controller design for reusable launch vehicles during reentry phase via compound adaptive fuzzy H-infinity control. Aerosp Sci Technol 72:36–48
2. Li MM, Jun Hu (2018) An approach and landing guidance design for reusable launch vehicle based on adaptive predictor-corrector technique. Aerosp Sci Technol 75:13–23
3. Wei CZ, Ju XZ, Wu R, He YF, Diao Y (2019) Geometry and time updaters-based arbitrary-yaw iterative explicit guidance for fixed-thrust boost back of vertical take-off/vertical landing reusable launch vehicles. Aerosp Sci Technol 95:105433
4. Jo B-U, Ahn J (2021) Optimal staging of reusable launch vehicles considering velocity losses. Aerosp Sci Technol 109:106431
5. Song Y, Miao XY, Cheng L, Gong SP (2021) The feasibility criterion of fuel-optimal planetary landing using neural networks. Aerosp Sci Technol 116:106860
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