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TOPOLOGY OPTIMIZATION OF MORPHING WING TRAILING EDGE BASED ON MULTI-POINTS DRIVING COMPLIANT MECHANISM

The wing is designed by specific flight conditions,and its aerodynamic efficiency under various conditions needs to be optimized.This paper studies the trailing edge of the morphing wing to make it meet the aerodynamic optimal deformation range under the premise of continuous smooth deformation.By u...

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Detaylı Bibliyografya
Asıl Yazarlar: KOU Xin, GE WenJie
Materyal Türü: Artigo
Dil:Chinês
Baskı/Yayın Bilgisi: Editorial Office of Journal of Mechanical Strength 2018-01-01
Seri Bilgileri:Jixie qiangdu
Konular:
Online Erişim:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.04.036
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