A case study on the modeling and simulation of UAVs

dc.authorid0000-0002-3065-1942
dc.authorid0000-0002-5743-3937
dc.authorid0000-0002-6106-2251
dc.authorid0000-0002-3065-1942
dc.authorid0000-0002-5743-3937
dc.contributor.authorKoç, Osman Kerem
dc.contributor.authorSertkaya, Ali
dc.contributor.authorGönül, Alişan
dc.contributor.authorTaner, Tolga
dc.contributor.authorDalkılıç, Ahmet Selim
dc.date.accessioned2024-07-22T11:54:56Z
dc.date.available2024-07-22T11:54:56Z
dc.date.issued2024
dc.departmentTeknik Bilimler Meslek Yüksekokulu
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.identifier.doi10.18186/thermal.1429773
dc.identifier.endpage174en_US
dc.identifier.issn2148-7847
dc.identifier.issue1en_US
dc.identifier.scopusqualityQ3
dc.identifier.startpage164en_US
dc.identifier.urihttps:/dx.doi.org/10.18186/thermal.1429773
dc.identifier.urihttps://hdl.handle.net/20.500.12451/12196
dc.identifier.volume10en_US
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.publisherYildiz Technical University
dc.relation.ispartofJournal of Thermal Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectANSYS
dc.subjectDesign
dc.subjectFlow Analysis
dc.subjectFluent
dc.subjectStructural Analysis
dc.subjectUnmanned Aerial Vehicles
dc.titleA case study on the modeling and simulation of UAVs
dc.typeArticle

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