The Adaptive Aspect Ratio Morphing Wing: Design Concept and Low Fidelity Skin Optimization
BKS Woods & MI Friswell (Swansea University)
Aerospace Science and Technology, Vol. 42, April-May 2015, pp. 209-217
This work introduces a new aircraft wing span morphing concept. Known as the Adaptive Aspect Ratio wing, this concept couples a compliant skin to a mechanism based internal structure to create a morphing wing capable of significant changes in span and aspect ratio. The technologies of the concept are first introduced and discussed. The compliant skin is established to be the dominant component in the design of this concept, requiring balancing of in-plane and out-of-plane stiffnesses. An initial skin design optimization exercise is performed using analytical models, providing insight into the interplay between the various parameters of the skin design.
This material has been published in the Aerospace Science and Technology, Vol. 42, April-May 2015, pp. 209-217, the only definitive repository of the content that has been certified and accepted after peer review. Copyright and all rights therein are retained by Elsevier.
Link to paper using doi: 10.1016/j.ast.2015.01.012
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