Flutter Analysis on Composite Rudder of Air-to-Air Missile

The flutter analysis model of composite rudder is established, and the flutter velocity at ambient temperature is calculated, the influence of the layup scheme on the flutter characteristics of the composite rudder is studied. The results show that the flutter velocity of the composite rudder is 575...

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Autor principal: Shen Pengfei, Wu Wei, Huang Yimin, Wei Zhongwei, Luo Chuyang, Pan Lijian
Formato: article
Lenguaje:ZH
Publicado: Editorial Office of Aero Weaponry 2021
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Acceso en línea:https://doaj.org/article/08e7820907c34c59bc5a2461bab21895
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