Open Access
| Issue |
E3S Web Conf.
Volume 233, 2021
2020 2nd International Academic Exchange Conference on Science and Technology Innovation (IAECST 2020)
|
|
|---|---|---|
| Article Number | 04009 | |
| Number of page(s) | 9 | |
| Section | MEA2020-Mechanical Engineering and Automation | |
| DOI | https://doi.org/10.1051/e3sconf/202123304009 | |
| Published online | 27 January 2021 | |
- Sickinger C, Herbeck L, Stroehlein T, et al. (2004) Lightweight deployable booms: design, manufacture, verification, and smart materials application. In: 55th International Astronautical Congress. Germany, DLR, 2054-2064. [Google Scholar]
- Puig L, Barton A, Rando N. (2010) Review a review on large deployable structures for astrophysics missions. Acta Astronautica, 67(1-2): 12-26. [Google Scholar]
- Wu J a B, Zhao Z A, Ren G A. (2013) Multibody analysis of the force in deploying booms. Journal of Guidance, Control, and Dynamics, 36(6): 1881-1885. [CrossRef] [Google Scholar]
- Sickinger C, Herbeck L, Breitbach E. (2006) Structural engineering on deployable CFRP booms for a solar propelled sailcraft. Acta Astronautica, 58(4): 185-196. [Google Scholar]
- Herbeck L, Eiden M, Leipold M, et al. (2000) Development and test of deployable ultra-light weight CFRP boom for a solar sail. In: European Conference on Spacecraft Structures. Germany, DLR. [Google Scholar]
- Hakkak F, Khoddam S. (2007) On calculation of preliminary design parameters for lenticular booms. Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering, 221(3): 377-384. [CrossRef] [Google Scholar]
- Christian M. (2020) Buckling and post-buckling of thin-walled composite laminated beams—a review of engineering analysis methods. Applied Mechanics Reviews, 72(2): 020802,1-36. [Google Scholar]
- Irwin R, Veen J V, Buchner-Santos E, et al. (2010) Low-mass deployable spacecraft booms. In: AIAA SPACE 2010 Conference & Exposition. Anaheim, California. [Google Scholar]
- Yu H, Wujun C, Ruixiong L, et al. (2016) Mechanical characteristics of deployable composite thin-walled lenticular tubes. Composite Structures, 153: 601-613. [Google Scholar]
- Li R-X, Chen W-J, Fu G-Y. (2012) Buckling Analysis and Experiment of Lenticular CFRP Thin-Walled Tube Space Boom under Axial Compression. Journal of Astronautics, 33(8): 1164-1170.(in Chinese) [Google Scholar]
- Chu Z Y, Lei Y. (2014) Design theory and dynamic analysis of a deployable boom. Mechanism and Machine Theory, 71: 126-141. [Google Scholar]
- Bai Jiangbo, Xiong J. (2014) Temperature effect on buckling properties of ultra-thin-walled lenticular collapsible composite tube subjected to axial compression. Chinese Journal of Aeronautics, 27(5): 1312-1317. [CrossRef] [Google Scholar]
- GUO Yizhu, YANG Haoyu, GUO Hongwei, LIU Rongqiang, LUO Ani. (2020) Analysis of mechanical properties of spatial thin-walled elastic extension bar. Journal of Harbin Institute of Technology, 52 (1): 107-112. (in Chinese) [Google Scholar]
- Timoshenko S P, Gere J M. (1961) Theory of elastic stability. McGraw-Hill Book Company, New York. [Google Scholar]
- Shen GL, Hu GK. (2006) Mechanics of Composite Materials. Tsinghua University Press, Beijing. (in Chinese) [Google Scholar]
- Yu H, Wujun C, Jifeng G, et al. (2017) A study of flattening process of deployable composite thin-walled lenticular tubes under compression and tension. Composite Structures, 168: 164-177. [Google Scholar]
- Luo S, Wang WB. (2020) Stability analysis of compressed spherical shell based on arc length method. Chinese Journal of Applied Mechanics, 37(1): 161-167, 479. [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.