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Experimental and Numerical Results of a Flapping Wing Four Bar Mechanism
Date
2017-01-13
Author
Şenol, Münire Gülay
Arıkan, Kutlu Bilge
Kurtuluş, Dilek Funda
Metadata
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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This paper exploresthedesign and testing ofa flapping wing four-bar mechanism. A four-bar linkage system kinematic analysis is introduced for flapping wing motion. Four-bar mechanism is activated by a servo motor which is driven by microcontroller. The wing undergoes apure flapping motion at afixed pitchangle. Force measurements are performed for hover modeby using a force transducer. In addition, 3D numericalanalyses are performed and the results are compared with the experimental measurements. Overall, CFD results showgood agreement with the experimental data.
Subject Keywords
Applied aerodynamics
URI
https://hdl.handle.net/11511/45979
DOI
https://doi.org/10.2514/6.2017-0498
Collections
Department of Aerospace Engineering, Conference / Seminar
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M. G. Şenol, K. B. Arıkan, and D. F. Kurtuluş, “Experimental and Numerical Results of a Flapping Wing Four Bar Mechanism,” 2017, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/45979.