Conceptual Conceptual study of a morphing winglet based on unsymmetrical stiffness

Wang Chen; Khodaparast Hamed Haddad; Friswell Michael I.

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Conceptual Conceptual study of a morphing winglet based on unsymmetrical stiffness

机译：基于不对称刚度的变形小翼的概念研究

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Morphing technology has the potential to increase aircraft performance. Among the morphing technologies, the morphing winglet is a promising solution due to its small size and large effect on the aerodynamics. Morphing winglets have to carry the spanwise aerodynamic loads, with low weight and small size. This makes the design of a reliable morphing structure of great importance to realize a morphing winglet.

机译：变形技术具有提高飞机性能的潜力。在变形技术中，变形小翼是一种有前途的解决方案，因为它的体积小且对空气动力学的影响很大。变形小翼必须承受重量轻，体积小的翼展方向气动载荷。这使得可靠的变形结构的设计对于实现变形小翼非常重要。

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来源
《Aerospace science and technology》 |2016年第11期|546-558|共13页
作者
Wang Chen; Khodaparast Hamed Haddad; Friswell Michael I.;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Conceptual study; Compliant structure; Morphing winglet; Unsymmetrical stiffness;

机译：概念研究;柔顺结构;变形小翼;不对称刚度;

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Conceptual Conceptual study of a morphing winglet based on unsymmetrical stiffness

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