Experimental and Numerical Results of a Flapping Wing Four Bar Mechanism

2017-01-13
Şenol, Münire Gülay
Arıkan, Kutlu Bilge
Kurtuluş, Dilek Funda
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.
Citation Formats
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.