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.
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
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