Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle

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MetadadosDescriçãoIdioma
Autor(es): dc.contributorNew Mexico State University-
Autor(es): dc.contributorNew Mexico Institute of Mining and Technology-
Autor(es): dc.contributorUniversidade Estadual Paulista (Unesp)-
Autor(es): dc.creatorLane, P.-
Autor(es): dc.creatorThroneberry, G.-
Autor(es): dc.creatorFernandez, I.-
Autor(es): dc.creatorHassanalian, M.-
Autor(es): dc.creatorVasconcellos, R. [UNESP]-
Autor(es): dc.creatorAbdelkefi, A.-
Data de aceite: dc.date.accessioned2022-02-22T00:27:11Z-
Data de disponibilização: dc.date.available2022-02-22T00:27:11Z-
Data de envio: dc.date.issued2020-12-11-
Data de envio: dc.date.issued2020-12-11-
Data de envio: dc.date.issued2020-09-01-
Fonte completa do material: dc.identifierhttp://dx.doi.org/10.3390/drones4030039-
Fonte completa do material: dc.identifierhttp://hdl.handle.net/11449/199371-
Fonte: dc.identifier.urihttp://educapes.capes.gov.br/handle/11449/199371-
Descrição: dc.descriptionThroughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, as these are two of the main challenges of these systems. Researchers have recently been turning towards bioinspiration as a way to enhance aerodynamic performance. In this work, the propulsion system of a flapping-wing micro air vehicle is investigated to identify the limitations and drawbacks of specific designs. Each system has a tandem wing configuration inspired by a dragonfly, with wing shapes inspired by a bumblebee. For the design of this flapping-wing, a sizing process is carried out. A number of actuation mechanisms are considered, and two different mechanisms are designed and integrated into a flapping-wing system and compared to one another. The second system is tested using a thrust stand to investigate the impact of wing configurations on aerodynamic force production and the trend of force production from varying flapping frequency. Results present the optimal wing configuration of those tested and that an angle of attack of two degrees yields the greatest force production. A tethered flight test is conducted to examine the stability and aerodynamic capabilities of the drone, and challenges of flapping-wing systems and solutions that can lead to successful flight are presented. Key challenges to the successful design of these systems are weight management, force production, and stability and control.-
Descrição: dc.descriptionConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)-
Descrição: dc.descriptionCoordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)-
Descrição: dc.descriptionDepartment of Mechanical and Aerospace Engineering New Mexico State University-
Descrição: dc.descriptionDepartment of Mechanical Engineering New Mexico Institute of Mining and Technology-
Descrição: dc.descriptionDepartment of Aeronautical Engineering São Paulo State University (Unesp), Campus of São João da Boa Vista-
Descrição: dc.descriptionDepartment of Aeronautical Engineering São Paulo State University (Unesp), Campus of São João da Boa Vista-
Descrição: dc.descriptionCNPq: 311082/2016-5-
Descrição: dc.descriptionCAPES: 88881.302889/2018-01-
Formato: dc.format1-18-
Idioma: dc.languageen-
Relação: dc.relationDrones-
???dc.source???: dc.sourceScopus-
Palavras-chave: dc.subjectBioinspiration-
Palavras-chave: dc.subjectFlapping wing system-
Palavras-chave: dc.subjectManufacturing-
Palavras-chave: dc.subjectTesting-
Título: dc.titleTowards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle-
Tipo de arquivo: dc.typelivro digital-
Aparece nas coleções:Repositório Institucional - Unesp

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