Bir İnsansız Hava Aracının Konvansiyonel Olmayan Esnek Kontrol Yüzeylerinin Yapısal Analizi ve İç Yapısının Tasarımı

Date

2014-06-18

Author

Arslan, Pınar
Uğur, Kalkan
Harun, Tıraş
İlhan Ozan, Tunçöz
Yosheph, Yang
Gürses, Ercan
Şahin, Melin
Özgen, Serkan
Yaman, Yavuz

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In this study, compliant and morphing unconventional control surfaces of an unmanned aerial vehicle (UAV) is examined. In this context, a compliant material for control surface is chosen and interior structure of the control surface is designed according to the selected material. During the design of an interior structure of the control surface, use of different number of servo actuators is taken into consideration. In consequence of material selection and design of the interior structure, it is shown that necessary deflection of the control surface is possible under the aerodynamic loads in flight conditions and servo actuation loads. Moreover, in this design, it is considered that compliant and morphing control surface and its interior structure is able to carry aerodynamic loads while sustaining the wing profile. As a result of various analyses, the safest number of servo actuators are decided to operate the control surface in a desired manner

Subject Keywords

Unconventional control surface, Structural analysis, Compliant materia

URI

https://hdl.handle.net/11511/80103

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

P. Arslan et al., “Bir İnsansız Hava Aracının Konvansiyonel Olmayan Esnek Kontrol Yüzeylerinin Yapısal Analizi ve İç Yapısının Tasarımı,” 2014, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/80103.