柔性弹丸飞行动力学研究

王良明

兵工学报 ›› 1998, Vol. 19 ›› Issue (3) : 208.

兵工学报 ›› 1998, Vol. 19 ›› Issue (3) : 208. DOI: 10.3969/j.issn.1000-1093.1998.03.004
论文

柔性弹丸飞行动力学研究

  • 王良明
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Flight Dynamics of Flexible Projectiles

  • Wang Liangming
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摘要

建立了大长细比弹丸刚体运动和柔性弯曲变形耦合的动力学模型;定义了柔性弹丸的平均弹轴系和刚体运动;以梁的弯曲理论为基础,推导了柔性弹丸的弯曲变形方程。在准静态变形条件下给出了柔性弹丸的攻角运动方程及其解,并由此获得了柔性弹丸的静态和动态稳定性条件,从中可看出柔性变形对 弹丸飞行稳定性的影响,为大长细比弹箭的设计提供了重要的理论依据。

Abstract

A dynamic coupled-model of the rigid-body motion and the flexible bending motion for a projectile having a large slenderness ratio is developed, and the mean axis and the rigid-boay motion of a flexible projectile are defined. Based on the theory of bending of a beam,equation of the bending deformation of a flexi?ble projectile is formulated. For the case of quasi-static deformation,the equation of attack of a flexible projectile and its analytic solution are obtained, and hence the conditions of static and dynamic stabilization are presented m the paper. The bend?ing effects are shown to lead to a decrease in the flight stability of finned projec?tiles.

关键词

弹丸 / 柔性变形 / 弹道学 / 稳定性理论

Key words

projectile / flexible bending deformation / aeroballistics / theory of staDiiization

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导出引用
王良明. 柔性弹丸飞行动力学研究. 兵工学报. 1998, 19(3): 208 https://doi.org/10.3969/j.issn.1000-1093.1998.03.004
Wang Liangming. Flight Dynamics of Flexible Projectiles. Acta Armamentarii. 1998, 19(3): 208 https://doi.org/10.3969/j.issn.1000-1093.1998.03.004

参考文献

[1] Timoshenko S,Young D Y,1Weaver W Jr. Vibration Problems in Engineering. 4th ed. John Wiley sons Inc. ,1974.
[2] 徐明友.火箭外弹道学.北京:国防エ业出版社,1980.
[3] 浦发.外弹道学.北京:国防エ业出版社,1980.

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