摘要
本文通过对鱼雷三自由度纵向姿态运动的分析,运用“固化系数法”,讨论得出入水鱼雷带空泡航行保持姿态运动稳定的条件。由此,提出入水鱼雷尾部稳定器设计原理思想,并初步论证了尾部稳定附件的功用和现实性。
The longitudinal motion attitude of a missile in three degrees of freedom was analyzed. On the basis of 'the solidified coefficient method', the conditions for stable flight of a water-entry missile running with cavity were obtained. Consequently, the basic idea of tail stabilizers designed for the water-entry missile was provided, their functions and realizability were proved elementally.
出处
《水动力学研究与进展（A辑）》
CSCD
北大核心
1990年第3期117-126,共10页
Chinese Journal of Hydrodynamics
关键词
鱼雷
入水
弹道
稳定
water-entry, trajectory, torpedo.
