A case study on the modeling and simulation of UAVs

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dc.authoridTaner, Tolga/0000-0002-3065-1942
dc.authoridGonul, Alisan/0000-0002-6106-2251
dc.authoridDalkilic, Ahmet Selim/0000-0002-5743-3937
dc.contributor.authorKoc, Osman Kerem
dc.contributor.authorSertkaya, Ali
dc.contributor.authorGonul, Alisan
dc.contributor.authorTaner, Tolga
dc.contributor.authorDalkilic, Ahmet Selim
dc.date.accessioned2024-12-24T19:30:31Z
dc.date.available2024-12-24T19:30:31Z
dc.date.issued2024
dc.departmentSiirt Üniversitesi
dc.description.abstractThe flow and structure of an application design for un-manned aerial vehicles (UAVs) are examined in this research. We also show an example of modeling and simulation study with the ANSYS Fluent and Mechanical programs. This research reveals the unmanned aerial vehicle's structural and mechanical design, structure configurations, energy-flow and struc-tural analysis, propulsion and firing systems, prototype production and testing, and design flow models. This study aims to complete the unmanned aerial vehicle design by determining its aerodynamic configurations. Due to the complexity of the design, a preliminary preparation for flow analysis is performed with simplified geometry as well as flow analysis. The unmanned aerial vehicle is tested at different velocities by numerical analysis. In addition, different density flow analyses provide predictions about the aerodynamic forces of the UAVs at different heights and temperatures. The thrust results are 4240 g, power became 1711.62 W with 2.48 g/W efficiency, and 12179 [rpm] revolution for 22.2 V voltage and 77.1 A current, respectively. The 5 different analyses are performed in the range of 2.9-12 million elements, and the solution meshes with the lowest number of elements by performing parametric studies with the ANSYS program that gives the most accurate result.
dc.description.sponsorshipTUBITAK (The Scientific and Technological Research Council of Turkey) Unmanned Aerial Vehicle Competition [548110]
dc.description.sponsorshipThis study was carried out as the flow analysis of the unmanned aerial vehicle, which was supported by the 2020 TUBITAK (The Scientific and Technological Research Council of Turkey) Unmanned Aerial Vehicle Competition (Project Funding Number 548110 and Date 15-20 September 2020) and was based on the altitude of Gaziantep.
dc.identifier.doi10.18186/thermal.1429773
dc.identifier.endpage174
dc.identifier.issn2148-7847
dc.identifier.issue1
dc.identifier.scopus2-s2.0-85184858001
dc.identifier.scopusqualityQ3
dc.identifier.startpage164
dc.identifier.trdizinid1259371
dc.identifier.urihttps://doi.org/10.18186/thermal.1429773
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/1259371
dc.identifier.urihttps://hdl.handle.net/20.500.12604/7550
dc.identifier.volume10
dc.identifier.wosWOS:001241341700001
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.publisherYildiz Technical Univ
dc.relation.ispartofJournal of Thermal Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_20241222
dc.subjectFlow Analysis
dc.subjectStructural Analysis
dc.subjectUnmanned Aerial Vehicles
dc.subjectFluent
dc.subjectDesign
dc.subjectANSYS
dc.titleA case study on the modeling and simulation of UAVs
dc.typeArticle

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