A review of dual-spin projectile stability

A review of dual-spin projectile stability
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DOI:
10.1016/j.dt.2019.06.003
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发表时间:
2020-02
期刊:
影响因子:
5.1
通讯作者:
James Norris;A. Hameed;J. Economou;Simon Parker
James Norris;A. Hameed;J. Economou;Simon Parker
中科院分区:
工程技术2区
文献类型:
--
作者:
James Norris;A. Hameed;J. Economou;Simon Parker

文献摘要

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本文对双自旋弹丸稳定性及其相关技术进行了简要的综述。它描述了如何修改传统的线性弹丸理论的稳定性因子,以更好地描述受控双自旋弹丸。最后,它回顾了研究受控双旋设计的不同方面如何影响飞行稳定性的工作,主要是机身结构和鸭翼特性。文中给出了结论,强调了所附讨论的重要指导方针。
This paper gives a succinct review of dual-spinprojectile stability and some technologies relating to them. It describes how the traditional stability factors from linear projectile theory are modified to better describe a controlled dual-spin projectile. Finally, it reviews works which have investigated how different aspects of a controlled dual-spin design can affect flight stability, primarily airframe structure and canard properties. A conclusion is given, highlighting important guidelines from the enclosed discussions.