Abstract:
可变形飞行器能自主地改变气动外形以适应不同的飞行任务,折叠翼是设计可变形飞行器最有前景的方案之一。本文建立了折叠翼的Z 形平面梁非线性动力学模型。
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Year: 2015
Page: 42-43
Language: Chinese
Cited Count:
WoS CC Cited Count: 0
SCOPUS Cited Count:
ESI Highly Cited Papers on the List: 0 Unfold All
WanFang Cited Count: -1
Chinese Cited Count:
30 Days PV: 5
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