Finite element method based structural analysis of quadcopter UAV chassis produced with 3D printer

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dc.contributor.authorAydın, Mustafa
dc.contributor.authorÇaşka, Serkan
dc.contributor.authorGök, Kadir
dc.contributor.authorÖzdemir, İkbal
dc.date.accessioned2023-03-22T19:48:25Z
dc.date.available2023-03-22T19:48:25Z
dc.date.issued2020
dc.departmentBelirleneceken_US
dc.description.abstractIn this study, the static analysis and manufacturing of a quadcopter type small unmanned aerialvehicle (UAV) design compatible with landing platforms was performed by using the finite elementmethod. In static analysis, the weight of the quadcopter body is considered as the load and the base isfixed. Each part of the quadcopter used in the Finite Element Analysis (FEA) is manufactured withAcrylonitrile Butadiene Styrene (ABS) and Polyactic Acid (PLA) materials with a thickness of 0.05mm with i3 prusa printer. As a result of the structural analysis, the stress produced in the quadcopterchassis produced from ABS material was 0,053 MPa and the stress on the quadcopter frame producedfrom PLA material was calculated as 0,065 MPa. In addition, the deformation in the quadcopter frameproduced from ABS material was 0,014 mm, while the quadcopter frame produced from PLA materialwas 0,010 mm.en_US
dc.identifier.endpage32en_US
dc.identifier.issn2687-6167
dc.identifier.issue44en_US
dc.identifier.startpage24en_US
dc.identifier.trdizinid395432en_US
dc.identifier.urihttps://hdl.handle.net/20.500.14034/1089
dc.identifier.urihttps://search.trdizin.gov.tr/yayin/detay/395432
dc.identifier.volume0en_US
dc.indekslendigikaynakTR-Dizinen_US
dc.language.isoenen_US
dc.relation.journalJournal of scientific reports-A (Online)en_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.titleFinite element method based structural analysis of quadcopter UAV chassis produced with 3D printeren_US
dc.typeArticleen_US

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