Aeroelastic Analysis of a Flapping Blow Fly Wing

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2020-06-01
Beker, Can
Turgut, Ali Emre
ARIKAN, KUTLUK BİLGE
Kurtuluş, Dilek Funda
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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
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In this study, a 3D model of the bio-inspired blowfly wing Callphere Erytrocephala is created and aeroelastic analysis is performed to calculate its aerodynamical characteristics by use of numerical methods. To perform the flapping motion, a sinusoidal input function is created. The scope of this study is to perform aeroelastic analysis by synchronizing computational fluid dynamics (CFD) and structural dynamic analysis models and to investigate the unsteady lift formation on the aeroelastic flapping wing for different angles of attack.
Micro air vehicle, Fluid-structure interaction analysis, Computational Fluid Dynamics, Structural dynamic analysis, Finite element analysis
https://hdl.handle.net/11511/70227
International Journal of Aviation Science and Technology
Department of Mechanical Engineering, Article

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Citation Formats
C. Beker, A. E. Turgut, K. B. ARIKAN, and D. F. Kurtuluş, “Aeroelastic Analysis of a Flapping Blow Fly Wing,” International Journal of Aviation Science and Technology, pp. 14–21, 2020, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/70227.
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