Structural analysis of the proposed multi-layer dodecarotor UAV

Basit Öğe Kaydı
dc.authorid0000-0002-3668-7591en_US
dc.authorid0000-0002-7149-3274en_US
dc.authorid0000-0002-1170-5327en_US
dc.contributor.authorÇabuk, Nihat
dc.contributor.authorYıldırım, Şahin
dc.contributor.authorBakırcıoğlu, Veli
dc.date.accessioned2022-08-25T09:55:39Z
dc.date.available2022-08-25T09:55:39Z
dc.date.issued2020en_US
dc.departmentBaşka Kurumen_US
dc.description.abstractIn this study, structural analysis of a multilayer dodecarotor drone system is presented. In the structural analysis performed with the finite element method, a multi-body analysis was performed for the major components that make up the system in order to see the effect of the contact forces at the joints due to assembly. In this way, the mechanical behavior of the material used for the main parts of the drone under the effect of the predicted forces was examined and its minimum requirements were determined. Among these parts, currently available carbon fiber materials were used for components with standard geometry. However, more specific components with non-standard geometry are produced by additive manufacturing method using Polylactic Acid material. The forces acting on the system was predicted by considering the propeller and motor properties to be used in the system and the stress, strain and displacements occurring in the components under these forces was examined. Finally, system strength has been discussed by presenting the obtained analysis results both graphically and numerically.en_US
dc.identifier.citationÇabuk, N., Yıldırım, Ş., Bakırcıoğlu, V. (2020). Structural analysis of the proposed multi-layer dodecarotor UAV. International Journal of Aeronautics and Astronautics, 1, (1), 18-22.en_US
dc.identifier.endpage22en_US
dc.identifier.issn2757-6574en_US
dc.identifier.issue1en_US
dc.identifier.startpage18en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12395/42985
dc.identifier.volume1en_US
dc.language.isoenen_US
dc.publisherSelçuk Üniversitesien_US
dc.relation.ispartofInternational Journal of Aeronautics and Astronauticsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Başka Kurum Yazarıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjectDroneen_US
dc.subjectMulti-copteren_US
dc.subjectStructural Analysisen_US
dc.subjectUnmanned Aerial Vehiclesen_US
dc.subjectÇoklu Helikopteren_US
dc.subjectYapısal Analizen_US
dc.subjectİnsansız Hava Araçlarıen_US
dc.titleStructural analysis of the proposed multi-layer dodecarotor UAVen_US
dc.typeArticleen_US

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
Küçük Resim
İsim:
Makale Dosyası.pdf
Boyut:
785.69 KB
Biçim:
Adobe Portable Document Format
Açıklama:
Makale Dosyası
İndir
Lisans paketi
Listeleniyor 1 - 1 / 1
Küçük Resim Yok
İsim:
license.txt
Boyut:
1.44 KB
Biçim:
Item-specific license agreed upon to submission
Açıklama:
İndir

Koleksiyon

Dergi Yayın Koleksiyonu