Analysis of the Nonlinear Rolling Motion of Finned Missiles

Author:

COHEN CHARLES J.1,CLARE THOMAS A.1,STEVENS FRANK L.1

Affiliation:

1. Naval Weapons Laboratory, Dahlgren, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 17 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A NEW CLOSED FORM SOLUTION FOR DYNAMIC STABILITY ANALYSIS OF ROLLING AIRFRAMES HAVING ONE PAIR ON-OFF ACTUATOR;Aviation;2021-08-19

2. Parameters estimation methodology for the nonlinear rolling motion of finned cylindrical body;Aerospace Science and Technology;2019-01

3. Experimental investigation of influence of strake wings on self-induced roll motion at high angles of attack;Chinese Journal of Aeronautics;2016-12

4. Flow control for suppression of self-excited rolling oscillation at high angles of attack;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-09-20

5. Experimental investigation of roll characteristics of a cruciform-finned slender body;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-08-06

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