Compliant structures based on stiffness asymmetry

Wang C.; Khodaparast H. H.; Friswell M. I.; Shaw A. D.

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Compliant structures based on stiffness asymmetry

机译：基于刚度不对称的柔顺结构

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One of the key problems in the development of morphing aircraft is the morphing structure, which should be able to carry loads and change its geometry simultaneously. This paper investigates a compliant structure, which has the potential to change the dihedral angle of morphing wing-tip devices. The compliant structure is able to induce deformation by unsymmetrical stiffness allocation and carry aerodynamic loads if the total stiffness of the structure is sufficient.

机译：变形飞机发展过程中的关键问题之一是变形结构，该结构应该能够承受载荷并同时改变其几何形状。本文研究了一种顺应性结构，它有可能改变变形翼尖装置的二面角。如果结构的总刚度足够，则顺应性结构能够通过不对称的刚度分配引起变形，并承受气动载荷。

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来源
《The Aeronautical Journal》 |2018年第1249期|442-161|共33页
作者
Wang C.; Khodaparast H. H.; Friswell M. I.; Shaw A. D.;
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作者单位

Swansea Univ, Coll Engn, Swansea, W Glam, Wales;

Swansea Univ, Coll Engn, Swansea, W Glam, Wales;

Swansea Univ, Coll Engn, Swansea, W Glam, Wales;

Swansea Univ, Coll Engn, Swansea, W Glam, Wales;

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正文语种 eng
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关键词
Morphing aircraft; compliant structure; corrugated panel; optimisation;

机译：变形飞机;柔性结构;波纹板;优化;

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Compliant structures based on stiffness asymmetry

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