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Numerical investigation of aerodynamic characteristics of free-spinning tail projectile with canards roll control
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.1 ) Pub Date : 2020-08-27 , DOI: 10.1177/0954410020953316
Jiawei Zhang 1 , Juanmian Lei 1 , Jianping Niu 1
Affiliation  

To reduce aerodynamic coupling between the canards and the tail fins of a canard-controlled projectile, the afterbody of the projectile is decoupled from the forebody by a bearing structure, namely...

中文翻译:

鸭翼侧倾控制自旋尾弹气动特性数值研究

为减少鸭翼控制炮弹的鸭翼和尾翼之间的空气动力耦合,炮弹的后体通过轴承结构与前体分离,即...
更新日期:2020-08-27
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