[1]陈施能.某型航空电子设备及安装架动力学分析[D].成都:电子科技大学,2007.
Chen Shineng.Dynamic Analysis for the Bracket of the Electronics Equipments and Aircraft[D].Chengdu:University of Electronic Science and Technology of China,2007.
[2]刘范川,任建锋,刘世刚.机载电子设备隔振系统固有频率的确定[J].电讯技术,2007,47(3):195-198.
Liu Fanchuan,Ren Jianfeng,Liu Shigang.Determining the free frequency of vibration isolation system for airborne electronic equipment[J].Telecommunication Engineering,2007,47(3):195-198.
[3]张军,谌勇,张志谊,等.整星隔振器的隔振性能分析[J].宇航学报,2005,26(增刊1):110-113.
Zhang Jun,Chen Yong,Zhang Zhiyi,et al.Performance analysis of the whole-spacecraft isolator[J].Journal of Astronautics,2005,26(S1):110-113.
[4]任建峰.电子设备结构动力响应研究中的关键技术[D].西安:电子科技大学,2006.
Ren Jianfeng.Key Techniques in the Research on the Dynamic Responses of the Electronic Equipments[D].Xi’an:University of Electronic Science and Technology of China,2006.
[5]刘衍平,高新霞,张刘斗.电子设备机柜随机振动试验的数值模拟[J].塑性工程学报,2007,14(4):151-155.
Liu Yanping,Gao Xinxia,Zhang Liudou.Numerical simulation tested to electronic equipment cabinet random vibrations[J].Journal of Plasticity Engineering,2007,14(4):151-155.
[6]Zarghamee M S.Optimum frequency of structures[J].AIAA Journal,1968,6(4):749-750.
[7]Pantelides C P,Tzan S R.Optimal design of dynamically constrained structures [J].Computers & Structures,1997,62(1):141-149.
[8]Tizzi S.A Ritz procedure for optimization of cylindrical shells,formed by a nearly symmetric and balanced angle-ply composite laminate,with fixed minimum frequency [J].Computers and Structures,2006,84(31):2159-2173.
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