摘要
以低速旋转的尾翼式火箭为研究对象 ,以梁的弯曲理论为基础 ,进行微元体和刚体的受力分析 ,推导出柔性火箭的弯曲变形方程 。
Based on the bending theory of beam, the forces acting on the rigid body and an element of a finned rocket with low spin rate are analyzed. The equation of bending deformation of a flexible rocket is formulated. A ballistic coupled model of the flight motion and the flexible bending motion is developed.
出处
《弹道学报》
CSCD
北大核心
2001年第1期50-55,61,共7页
Journal of Ballistics
