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大长径比弹箭飞行中的共振条件研究
引用本文:王良明,王中原,易文俊.大长径比弹箭飞行中的共振条件研究[J].弹道学报,2001,13(4):51-54.
作者姓名:王良明  王中原  易文俊
作者单位:南京理工大学弹道研究所,
摘    要:从弹簧空间摆动和弹性振动耦合的动力学模型出发,对弹箭飞行过程中的共振不稳定性问题进行了研究。在非动态耦合的情况下,得到了一阶弹性振动的共振频率和共振条件。在考虑动态耦合时,推导了一阶振动模态下的频率方程,建立了用于求解N阶振动模态下共振频率的特征矩阵。

关 键 词:飞行稳定性  共振  弹道学  大长径比飞行体  火箭  杆式穿甲弹
修稿时间:2001年4月11日

RESONANCE UNSTABILITY IN BALLISTICS OF FLEXIBLE BODY
Wang Liangming,Wang Zhongyuan,Yi Wengjun.RESONANCE UNSTABILITY IN BALLISTICS OF FLEXIBLE BODY[J].Journal of Ballistics,2001,13(4):51-54.
Authors:Wang Liangming  Wang Zhongyuan  Yi Wengjun
Abstract:Based on the coupled dynamic model for the spatial rotation and elastic vibration of a body, the resonance unstability of projectiles in flight is studied in the paper. Without regard to the dynamic uncoupling, the resonance frequencies and resonance conditions of the first order elastic vibration is obtained. And under the consideration of the dynamic uncoupling, the frequency equation with the first order mode is derived, also the characteristic matrix used for solution of resonance frequency with N modes is determined. The results are of great importance to design of projectiles or rockets with large L/D ratio.
Keywords:projectiles or rockets  flight stability  resonance  ballistics
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