MDAO fo Aerodynamic Assessment of a Morphed Wing for the Loiter Segment of a UAV Flight Mission

2016-01-08
Yang, Yosheph
Özgen, Serkan
Yaman, Yavuz
Ciarella, Andrea
Hahn, Marco
Beaverstock, Christhopher
Friswell, Michael

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In this paper a detailed overview of a framework for an optimization of a morphing wing is presented. The framework presented here aids the design process of a morphing UAV wing which includes the variety of the flight phases and morphing concepts. The framework consists of two main solvers to compute the aerodynamic assessment of the wing: a fast low-fidelity module that solves the aeroelastic problem by coupling a geometrically nonlinear structural model to a potential flow aerodynamic model and a high-fi...
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Citation Formats
Y. Yang et al., “MDAO fo Aerodynamic Assessment of a Morphed Wing for the Loiter Segment of a UAV Flight Mission,” 2016, Accessed: 00, 2021. [Online]. Available: www.aiaa.org/scitech2016.