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Akademický článek

Structure design of variable camber wing trailing edge based on multi-block rotating mechanism

Autor: SHI Xintong, YANG Yu, GE Wenjie, WANG Zhigang, SUN Xiasheng

Publikováno v: Xibei Gongye Daxue Xuebao, Vol 41, Iss 5, Pp 942-949 (2023)

The variable camber trailing edge enables the aircraft to maintain the best aerodynamic performance throughout the flight envelope, so as to achieve the ultimate goal of reducing aircraft fuel consumption and air pollutant emissions. It is one of the

Externí odkaz: https://doaj.org/article/e9e891af439f4ee6b1e56d0a51a51a3f

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Akademický článek

A skin design method of variable camber wing trailing edge

Autor: ZHANG Yonghong, TANG Shuangquan, WANG Miao, WANG Chengmin, GE Wenjie

Publikováno v: Xibei Gongye Daxue Xuebao, Vol 41, Iss 2, Pp 329-337 (2023)

As an important part of the wing, the skin deformation accuracy directly affect the aerodynamic performance of the aircraft in different environments. Based on the idea of easy processing and easy deformation, a method for designing variable section

Externí odkaz: https://doaj.org/article/eaac7a17bb754f22ad67f9f5386e6a21

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Akademický článek

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

Autor: KOU Xin, GE WenJie

Publikováno v: Jixie qiangdu, Vol 40, Pp 983-986 (2018)

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

Externí odkaz: https://doaj.org/article/5bfbf8e117994caabdad60dc8b41eb70

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