Flutter Mechanism Analysis for Circular Solar Sail

太阳帆 颤振 机制(生物学) 航空航天工程 机械 物理 天体生物学 气象学 工程类 航空学 空气动力学 航天器 量子力学
作者
Yingjing Qian,Lian-En Zuo,Zixiao Liu,Xiao-Dong Yang,Lei Xu
出处
期刊:AIAA Journal [American Institute of Aeronautics and Astronautics]
卷期号:61 (1): 497-504 被引量:1
标识
DOI:10.2514/1.j061994
摘要

No AccessTechnical NotesFlutter Mechanism Analysis for Circular Solar SailYing-Jing Qian, Lian-En Zuo, Zi-Xiao Liu, Xiao-Dong Yang and Lei XuYing-Jing QianBeijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, Beijing University of Technology, 100124 Beijing, People’s Republic of China*Professor, Faculty of Materials and Manufacturing.Search for more papers by this author, Lian-En ZuoBeijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, Beijing University of Technology, 100124 Beijing, People’s Republic of China†Graduate Student, Faculty of Materials and Manufacturing.Search for more papers by this author, Zi-Xiao Liu https://orcid.org/0000-0003-1161-1803University of California, Los Angeles, Los Angeles, California 90095‡Graduate Student, Department of Materials Science and Engineering.Search for more papers by this author, Xiao-Dong YangBeijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, 100124 Beijing, People’s Republic of China§Professor, Faculty of Materials and Manufacturing.Search for more papers by this author and Lei XuBeijing Spacecrafts, 100094 Beijing, People’s Republic of China¶Senior Engineer.Search for more papers by this authorPublished Online:27 Nov 2022https://doi.org/10.2514/1.J061994SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Liu Z. 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C. and Miyazaki Y., “Effect of Static and Dynamic Solar Sail Deformation on Center of Pressure and Thrust Forces,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2006-6184, 2013. https://doi.org/10.2514/6.2006-6184 Google Scholar[26] Kabe A. M. and Sako B. H., “Vibration of Continuous Systems,” Structural Dynamics Fundamentals and Advanced Applications, Vol. 2, Academic Press, California, 2020, pp. 749–945. https://doi.org/10.1016/B978-0-12-821615-6.00009-5 Google Scholar[27] Murphy D. M., Murphey T. W. and Gierow P. A., “Scalable Solar-Sail Subsystem Design Concept,” Journal of Spacecraft and Rockets, Vol. 40, No. 4, July 2003, pp. 539–547. https://doi.org/10.2514/2.3975 LinkGoogle Scholar[28] Wie B., “Solar Sail Attitude Control and Dynamics, Part 1,” Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4, July 2004, pp. 526–535. https://doi.org/10.2514/1.11134 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byStudy Membrane Solarelasticity Using a Wave Model and a Corpuscular Model of LightJinduo Chen, Aiming Shi , Yiwen He, Earl H. Dowell, Kuanfang Ren, Yang Pei and Haitao Zhang1 June 2023 | AIAA Journal, Vol. 61, No. 9 What's Popular Volume 61, Number 1January 2023 CrossmarkInformationCopyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsDynamic AnalysisMaterials and Structural MechanicsPropulsion and PowerSpacecraft PropulsionStructural Dynamics and Characterization KeywordsSolar SailFlutter AnalysisModal AnalysisAcknowledgmentsThis work was supported in part by the National Natural Science Foundation of China (project numbers 12172013 and 11772009) and the State Key Laboratory of Mechanical System and Vibration (grant number MSV202107). The data that support the plots within this paper and other finding of this study are available from the corresponding author on request.PDF Received27 April 2022Accepted31 October 2022Published online27 November 2022
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