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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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Journal of Mechanical Strength
2017-01-01
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| Series: | Jixie qiangdu |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.040 |
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