翼
尺寸
空气动力学
气动弹性
纵横比(航空)
机翼载荷
还原(数学)
折叠(DSP实现)
铰链
阻力
航空航天工程
升力诱导阻力
结构工程
工程类
副翼
航程(航空)
升阻比
攻角
材料科学
数学
几何学
艺术
复合材料
视觉艺术
作者
Huaiyuan Gu,Fintan Healy,Djamel Rezgui,Jonathan E. Cooper
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2022-11-28
卷期号:60 (2): 461-475
被引量:11
摘要
High-aspect-ratio wings are of particular interest to modern aircraft design due to the inherent reduction in induced drag that they provide. However, such wing configurations often come with problems such as increased structural weight and oversized wingspans for existing airport facilities. Unlike conventional folding wingtips, as used on the 777-X, this paper demonstrates the use of semi-aeroelastic hinge devices that enable aircraft incorporating high-aspect-ratio wings not only to fit into airport gates, but also to alleviate aerodynamic loads by allowing floating wingtips to be used in-flight. This study establishes a preliminary design process for such a wing configuration and undertakes a comprehensive sizing process to investigate the impact of the device on wing weight and aircraft performance. For the cases considered, a reduction in wing weight of approximately 25% can be achieved by utilizing the semi-aeroelastic hinge, which can lead to more than 5% improvement in aircraft range.
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