The aerodynamic characteristics and its estimation method of finned missile experiencing spin-deformation coupling motion
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference34 articles.
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4. Flight motion of a continuously elastic finned missile;Murphy;J. Guid. Control Dyn.,2003
5. Magnus characteristics of finned and nonfinned projectiles;Platou;AIAA J.,1965
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