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- W2183778041 abstract "An analytical aeroelastic model to investigate the aeroelastic stability of a span morphing aircraft is derived. Structural and aeroelastic models are derived with the parameteric variations introduced by a span morphing wing. Dynamic aeroelastic stability analysis is performed with thin airfoil theory and CFD. A CFD analysis of span morphing shows the lift increases in a non-linear fashion during the morphing process, and after the morphing is completed. The utter analysis, based on the CFD results, shows a signicant reduction in utter velocity during morphing due to inertial, elastic and aerodynamic variations, and due to the ow evolution after the morphing period. This study shows that the development of low delity aeroelastic models of morphing wings, supplemented with high delity analysis, can quantify the phenomena associated with the morphing and also serve as precursor to a computationally expensive, fully coupled high delity simulation of utter due to morphing." @default.
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- W2183778041 date "2014-01-01" @default.
- W2183778041 modified "2023-09-27" @default.
- W2183778041 title "Aeroelastic Modeling of Morphing Aircraft Wings" @default.
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