Journal of Shanghai Jiaotong University ›› 2016, Vol. 50 ›› Issue (01): 145-151.
Previous Articles Next Articles
CAI Qiyao1,CHEN Wujun1,ZHANG Daxu1,PENG Fujun2,FANG Guangqiang2
Received:
2014-12-18
Online:
2016-01-29
Published:
2016-01-29
CLC Number:
CAI Qiyao1,CHEN Wujun1,ZHANG Daxu1,PENG Fujun2,FANG Guangqiang2. Buckling Analysis and Experiment of Cantilever ThinWalled Lenticular CFRP Space Boom[J]. Journal of Shanghai Jiaotong University, 2016, 50(01): 145-151.
[1]陈务军.空间可展结构体系与分析导论[M].北京:中国宇航出版社,2006:150. [2]白江波,熊峻江,高军鹏,等.可折叠复合材料豆荚杆的制备与验证[J].航空学报,2011,32(7):12171223. BAI Jiangbo, XIONG Junjiang, GAO Junpeng, et al. Fabrication and validation of collapsible composite lenticular tubes [J]. Acta Aeronautica et Astronautica Sinica, 2011,32(7):12171223. [3]房光强,彭福军.航天器可展开支撑杆的研制及其收拢展开特性研究[J].材料工程,2009(增刊2):157160. FANG Guangqiang, PENG Fujun. Fabrication and retraction/deployment testing of space deployable booms[J]. Journal of Material Engineering, 2009(Sup 2): 157160. [4]董志强,段宝岩.星载天线缠绕肋条的力学特性研究[J].西安电子科技大学学报,2001,28(6):755758. DONG Zhiqiang, DUAN Baoyan. Study of the behavior mechanics of the extendible satellite antenna with the type of twinning ribs [J]. Journal of Xidian University, 2001, 28(6): 755758. [5]李瑞雄,陈务军,付功义,等.透镜式缠绕肋压扁缠绕过程数值模拟分析[J].宇航学报,2011,32(1): 224231. LI Ruixiong, CHEN Wujun, FU Gongyi. Numerical simulation of flattening and wrapping process of lenticular wrappedrib [J]. Journal of Astronautics, 2011, 32(1): 224231. [6]李瑞雄,陈务军,付功义,等.透镜式缠绕肋压扁缠绕过程数值模拟及参数研究[J].工程力学,2011,28(11):244250. LI Ruixiong, CHEN Wujun,FU Gongyi,et al. Numerical simulation and parametric study on flattening and wrapping process of lenticular wrappedrib[J]. Engineering of Mechanics, 2011, 28(11):244250. [7]邹涛,陈务军,彭福军,等.透镜式缠绕肋收展过程数值模拟分析[J].哈尔滨工程大学学报,2013,34(2):151156. ZOU Tao, CHEN Wujun, PENG Fujun, et al.Numerical simulation of stowing and deploying process of lenticular wrappedrib [J]. Journal of Harbin Engineering University, 2013,34(2):151156. [8]李瑞雄,陈务军,付功义.透镜式薄壁CFRP 管空间伸展臂轴压屈曲分析及试验[J].宇航学报,2012,33(8): 11641170. LI Ruixiong, CHEN Wujun, FU Gongyi.Buckling analysis and experiment of lenticular CFRP thinwalled tube space boom under axial compression[J]. Journal of Astronautics, 2012,33(8):11641170. [9]刘锦贤. 空间可展天线支撑结构热结构分析[D].上海:上海交通大学研究生院,2013. [10]SICKINGER C, HERBECK L, BREITBACH E. Structural engineering on deployable CFRP booms for a solar propelled sail craft[C]//The 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. Bremen, Germany: Acta Astronautica, 2003. [11]IRWIN R J, VANDER VEEN J A, BuchnerSantos E, et al. Lowmass deployable spacecraft booms[C]//AIAA SPACE 2010 Conference & Exposition. Anaheim, California: AIAA, 2010. [12]MARCO Straubel, JOACHIM Block, MICHAEL Sinapius, et al. Deployable composite booms for various gossamer space structures[C]//The 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Denver, Colorado: AIAA, 2011. [13]庄茁,由小川,廖剑晖,等. 基于ABAQUS的有限元分析和应用[M]. 北京:清华大学出版社,2009. |
[1] | CAI Qiyao1,CHEN Wujun1,ZHANG Daxu1,PENG Fujun2,FANG Guangqiang2. Numerical Simulation and Flattening Tests of Compression and Pulling of Lenticular ThinWalled Tubular Space Booms [J]. Journal of Shanghai Jiaotong University, 2016, 50(04): 601-607. |
[2] | CAI Qiyao1,CHEN Wujun1,ZHANG Daxu1,PENG Fujun2,FANG Guangqiang2. Mechanical Behavior Analysis and Experiment of Kapton Film Folding [J]. Journal of Shanghai Jiaotong University, 2014, 48(08): 1109-1115. |
[3] | HUANG Haojie1,ZHANG Junqi2,LIU Longquan2,WANG Hai2. Stress Analysis of Composite Curved Laminate Under Loading [J]. Journal of Shanghai Jiaotong University, 2014, 48(08): 1116-1121. |
[4] | LI Zhen, CHEN Xiu-Hua, WANG Hai. Buckling Optimization of Composite Laminate Using Modified Ant Colony Optimization [J]. Journal of Shanghai Jiaotong University, 2012, 46(05): 768-773. |
[5] | LI Wei-Ming, HONG Jia-Zhen. Research on Model Updating Method Based on Frequency Response Functions [J]. Journal of Shanghai Jiaotong University, 2011, 45(10): 1455-1459. |
[6] | CHAI Xianghai,ZHANG Zhinan,YAN Jun,LIU Chuanxin. Lightweight Design for Improving Aeroengine Fan Blade Impact Resistance Capability [J]. Journal of Shanghai Jiaotong University, 2020, 54(2): 186-192. |
Viewed | ||||||||||||||||||||||||||||||||||||||||||||||||||
Full text 184
|
|
|||||||||||||||||||||||||||||||||||||||||||||||||
Abstract 1235
|
|
|||||||||||||||||||||||||||||||||||||||||||||||||