[1] Castanié B, Bouvet C, Aminanda Y, et al. Modeling of low-energy/low-velocity impact on Nomex honeycomb sandwich structures with metallic skins[J]. International Journal of Impact Engineering, 2008, 35(7): 620-634.
[2] Foo C C, Chai G B, Seah L K. Mechanical properties of Nomex material and Nomex honeycomb structure[J]. Composite Structures, 2007, 80: 588-594.
[3] Gornet L, Marguet S, Marckmann G. Modeling of Nomex honeycomb cores, linear and nonlinear behaviors[J]. Mechanics of Advanced Materials and Structures, 2007, 14(8): 589-601.
[4] Zhang Xiaozhen, Li Yong, Song Guizhi, et al. The effect temperature on compression strength and shear strength of Nomex honeycomb[J]. Material Engineering, 1993(10): 17-18. (in Chinese)
[5] Sun Chengwei, Lu Qisheng, Fan Zhengxiu, et al. Laser Irradiation Effect[M]. Beijing: National Defense Industry Press, 2002. (in Chinese)
[6] Li Jiaju, Yang Guicheng. The progression and determination of elastic constants of honeycomb sandwich panels[J]. Fiber Reinforced Plastics/Composites, 1992, 5: 6-13. (in Chinese)
[7] The Institute of Mechanics of the Chinese Academy of Science. Bending of Laminated Plate and Shell Stability and Vibration[M]. Beijing: Science Press, 1977. (in Chinese)
[8] Yuan Jiajun. Design and Analysis of Satellite Structures [M]. Beijing: China Astronautic Publishing House, 2004. (in Chinese)