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- W2161140897 abstract "The morphing concept for unmanned aerial vehicles is a topic of current research interest in aerospace engineering. One concept of morphing is to change the wing configuration during flight to allow for multiple flight regimes. A particular approach to planform morphing is a variable-span morphing wing to increase wingspan to reduce induced drag and increase range and endurance. The wing area and the aspect ratio of the variable-span morphing wing increase as the wingspan increases. This means that the total lift increases while the induced drag is reduced, whereas the wing-root bending moment increases, thus, requiring a larger bending stiffness of the wing structure. Therefore, a study of the variable-span morphing wing requires not only aerodynamic analysis but also an investigation of the aeroelastic characteristics of the wing. The aerodynamic characteristics of the variable-span morphing wing are investigated, and a static aeroelastic analysis is performed." @default.
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- W2161140897 date "2005-03-01" @default.
- W2161140897 modified "2023-10-02" @default.
- W2161140897 title "Aerodynamic and Static Aeroelastic Characteristics of a Variable-Span Morphing Wing" @default.
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- W2161140897 doi "https://doi.org/10.2514/1.4397" @default.
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