Aeroelastic behaviour of UAV wings due to morphing

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2017-01-01
Unlusoy, Levent
Yaman, Yavuz
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Purpose - The purpose of this paper is to analyse the effects of morphing on the aeroelastic behaviour of unmanned aerial vehicle (UAV) wings to make an emphasis on the required aeroelastic tailoring starting from the conceptual design of the morphing mechanisms.
Flutter prediction, Morphing wings, Pk-method, State-space solution, Thodorsen aerodynamics, Typical section model
https://hdl.handle.net/11511/36561
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Department of Aerospace Engineering, Article

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Citation Formats
L. Unlusoy and Y. Yaman, “Aeroelastic behaviour of UAV wings due to morphing,” AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, pp. 30–38, 2017, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/36561.
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