Design and experiment of honeycomb sandwich plate of optical small satellite

Jiang Quan; Yang Hongbo; Li Zongxuan; Zhang Lei

doi:10.3788/irla201645.1235001

[1] Gu Song, Liu Chunyu, Jia Xuezhi. Integerated design of bus and payload structure of small optical remote sensing satellite[J]. Optics and Precision Engineering, 2013, 21(12): 207-214. (in Chinese)

[2] An Yuan, Jia Xuezhi, Zhang Lei, et al. Optimizing design of CFRP based main backbone with high stiffness ratio for space camera[J]. Optics and Precision Engineering, 2013, 21(2): 416-422. (in Chinese)

[3] Gibson L J, Ashby M F. Cellular Solids Structure and Properties[M]. 2nd ed. Cambridge: Cambridge University Press, 1997.

[4] Zhang Weihong, Duan Wengdong, Xu Yingjie, et al. Forecast of equivalent outplane shear modulus and size effect for honeycomb sandwich panels[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(2): 288-292. (in Chinese)

[5] Zhang Tieliang, Ding Yunliang, Jin Haibo, et al. Comparative analysis of equivalent models for honeycomb sandwich plate[J]. Chinese Journal of Applied Mechanics, 2011, 28(3): 275-282. (in Chinese)

[6] Jiang Dong, Jiang Zhiyuan, Fei Qingguo, et al. Dynamic characteristics of honeycomb sandwich composite considering effect of adhesive layer[J]. Journal OF Southeast University, 2013, 43(5): 1068-1073. (in Chinese)

[7] Jiang D, Zhang D H, Fei Q G, el al. An approach on identification of equivalent properties of honeycomb core using experimental modal data[J]. Finte Elements in Analysis and Design, 2014, 90: 84-92.

[8] Ding Ling, Sun Hui, Jia Hongguang, et al. Optimization design of composite wing skin with honeycomb sandwich by genetic algorithm[J]. Optics and Precision Engineering, 2014, 22(12): 3272-3279. (in Chinese)

[9] Wang Dongfang, Yang Jialing. Analysis of the performance of a beam made of composite materials with a glue layer[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9): 1655-1663. (in Chinese)

[10] Zhang Jiajia, He Jingwu. Simulation and investigation for effect of adhesive in honeycomb sandwich panels[J]. Aircraft Design, 2008, 28 (6): 27-30. (in Chinese)

[11] Tanimoto Y, Nishiwaki T, Shiomi T, et al. A numerical modeling for eigenvibration analysis of honeycomb sandwich panels[J]. Composite Interfaces, 2001, 8(6): 393-402.

[12] Liu Jingbo, Du Xiuli. Structural Dynamic[M]. Beijing: China Machine Press, 2005: 60-61. (in Chinese)

[13] Dong Deyi, Xin Hongwei, Yang Liwei, et al. Random vibration analysis and its verification for large aperture mirror component[J]. Journal of Vibration And Shock, 2011, 30(11): 74-78. (in Chinese)