节点文献
小型弹箭惯性矩的测定
The Measurement of Moment of Inertia for Small Missiles
【摘要】 叙述了三线摆的结构原理 ,介绍了该摆小角与大角摆动周期的计算方法。利用三线摆的结构原理可以测量小型弹箭、子弹头、飞机模型及其他构件的惯性矩。当 R/ L <1 / 30 ,φ0 ≤ 60°时 ,该装置的测量精确度可优于 1 %。
【Abstract】 The structure principle of three line pendulum is outlined,and the calculation methods of its shimmy period in small and large angle are presented.The structure principle of three line pendulum can be used to measure the moment of inertia of small missiles,submunition,aeroplane model and other structural members.When R/L<1/30,and φ 0≤60°,the measurement accuracy can be better than 1%.
【关键词】 单兵导弹;
三线摆;
惯性矩;
摆动周期;
【Key words】 Shoulder launched Missile; Tree line pendulum; Moment of inertia; Swing period.;
【Key words】 Shoulder launched Missile; Tree line pendulum; Moment of inertia; Swing period.;
- 【文献出处】 导弹与航天运载技术 ,Missiles and Space Vehicles , 编辑部邮箱 ,2001年04期
- 【分类号】V414
- 【下载频次】42