Experimental and numerical results of a flapping wing four bar mechanism
| dc.authorscopusid | 55888184200 | |
| dc.authorscopusid | 24438001000 | |
| dc.authorscopusid | 15837320400 | |
| dc.contributor.author | Arıkan, Kutluk Bilge | |
| dc.contributor.author | Arikan,K.B. | |
| dc.contributor.author | Kurtulus,D.F. | |
| dc.contributor.other | Department of Mechatronics Engineering | |
| dc.date.accessioned | 2024-07-05T15:44:53Z | |
| dc.date.available | 2024-07-05T15:44:53Z | |
| dc.date.issued | 2017 | |
| dc.department | Atılım University | en_US |
| dc.department-temp | Senol M.G., Department of Aerospace Engineering, Middle East Technical University, Aerospace Engineering Department, Ankara, 06800, Turkey; Arikan K.B., Department of Mechatronic Engineering, Mechatronic Engineering, Atilim University, Ankara, 06836, Turkey; Kurtulus D.F., Department of Aerospace Engineering, Middle East Technical University, Aerospace Engineering Department, Ankara, 06800, Turkey | en_US |
| dc.description.abstract | This paper explores the design and testing of a 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 a pure flapping motion at a fixed pitch angle. Force measurements are performed for hover mode by using a force transducer. In addition, 3D numerical analyses are performed and the results are compared with the experimental measurements. Overall, CFD results show good agreement with the experimental data. © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. | en_US |
| dc.identifier.citation | 1 | |
| dc.identifier.doi | 10.2514/6.2017-0498 | |
| dc.identifier.isbn | 978-162410447-3 | |
| dc.identifier.scopus | 2-s2.0-85017281907 | |
| dc.identifier.uri | https://doi.org/10.2514/6.2017-0498 | |
| dc.identifier.uri | https://hdl.handle.net/20.500.14411/3839 | |
| dc.language.iso | en | en_US |
| dc.publisher | American Institute of Aeronautics and Astronautics Inc. | en_US |
| dc.relation.ispartof | AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting -- 55th AIAA Aerospace Sciences Meeting -- 9 January 2017 through 13 January 2017 -- Grapevine -- 126423 | en_US |
| dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
| dc.rights | info:eu-repo/semantics/closedAccess | en_US |
| dc.subject | [No Keyword Available] | en_US |
| dc.title | Experimental and numerical results of a flapping wing four bar mechanism | en_US |
| dc.type | Conference Object | en_US |
| dspace.entity.type | Publication | |
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