UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT

UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT

In order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. First,a kinetic equation based on Lagrange’ s Equation was established,which provided a theoretic base for the simulation. Then,related...

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Bibliographic Details
Main Authors: LIU DuanChen, HAN XueFeng, ZHANG Yue, ZHANG MingYue, LIU XiaoDong
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2017-01-01
Series:Jixie qiangdu
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.040
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