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Performance Determination of Axial Wind Tunnel Fan with Reverse Engineering, Numerical and Experimental Methods

dc.authorscopusid 57193872973
dc.authorscopusid 55371892800
dc.authorwosid Kocak, Eyup/Hik-2192-2022
dc.authorwosid Ayli, Ulku Ece/J-2906-2016
dc.contributor.author Kocak, Eyup
dc.contributor.author Koçak, Eyup
dc.contributor.author Ayli, Ece
dc.contributor.authorID 283455 tr_TR
dc.contributor.authorID 265836 tr_TR
dc.contributor.other Makine Mühendisliği
dc.date.accessioned 2024-05-08T08:22:24Z
dc.date.available 2024-05-08T08:22:24Z
dc.date.issued 2022
dc.department Çankaya University en_US
dc.department-temp [Kocak, Eyup; Ayli, Ece] Cankaya Univ, Dept Mech Engn, TR-06810 Ankara, Turkey en_US
dc.description.abstract In today's technology, in case of the need for rehabilitation, renovation, or damage, it is necessary to recover the problems quickly with a cost-effective approach. In the case of destructive failure, or misdesign of the devices, replacing the problematic part with the new design is crucial. In order to substitute the related part with the efficient one, reverse engineering (RE) methodology is utilized. In this paper, from the perspective of engineering implementation and based on the idea of reverse engineering, axial wind tunnel fan is rehabilitated using numerical and experimental methods. The current study is focused on an axial pressurization fan placed into Cankaya University Mechanical Engineering Laboratory wind tunnel that has firm guaranteed specifications of 5.55 m(3)/s airflow capacity. The measurements performed during experiments showed that the fan provides less than 60% airflow compared with firm guaranteed specifications. In order to determine the problems of the existing fan, a reverse engineering methodology is developed, and the noncontact data acquisition method is used to form a computer aided drawing (CAD) model. A computational fluid dynamics (CFD) methodology is developed to analyze existing geometry numerically, and results are compared with an experimental study to verify numerical methodology. According to the results, the prediction accuracy of the numerical method can attain 92.95% and 96.38% for flowrate and efficiency, respectively, at the maximum error points. en_US
dc.description.publishedMonth 8
dc.description.sponsorship Tubitak [2209-A] en_US
dc.description.sponsorship The construction of the setup is financially supported by Tubitak 2209-A. The reverse engineering studies are performed at TOBB ETU Hydro Energy Research Center CFD Laboratory. en_US
dc.description.woscitationindex Science Citation Index Expanded
dc.identifier.citation Koçak, Eyup; Aylı, Ece. (2022). "Performance Determination of Axial Wind Tunnel Fan with Reverse Engineering, Numerical and Experimental Methods", Journal of Computing and Information Science in Engineering, Vol.22, No.4. en_US
dc.identifier.doi 10.1115/1.4053672
dc.identifier.issn 1530-9827
dc.identifier.issn 1944-7078
dc.identifier.issue 4 en_US
dc.identifier.scopus 2-s2.0-85124899559
dc.identifier.scopusquality Q2
dc.identifier.uri https://doi.org/10.1115/1.4053672
dc.identifier.volume 22 en_US
dc.identifier.wos WOS:000821145700014
dc.identifier.wosquality Q3
dc.language.iso en en_US
dc.publisher Asme en_US
dc.relation.publicationcategory Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı en_US
dc.rights info:eu-repo/semantics/closedAccess en_US
dc.scopus.citedbyCount 1
dc.subject Blade en_US
dc.subject Axial Fan en_US
dc.subject Reverse Engineering en_US
dc.subject Cfd en_US
dc.subject Rehabilitation en_US
dc.subject Wind Tunnel en_US
dc.subject Experiment en_US
dc.title Performance Determination of Axial Wind Tunnel Fan with Reverse Engineering, Numerical and Experimental Methods tr_TR
dc.title Performance Determination of Axial Wind Tunnel Fan With Reverse Engineering, Numerical and Experimental Methods en_US
dc.type Article en_US
dc.wos.citedbyCount 1
dspace.entity.type Publication
relation.isAuthorOfPublication 6ad744ba-3168-41f4-8cc1-ca6ed3c10eee
relation.isAuthorOfPublication.latestForDiscovery 6ad744ba-3168-41f4-8cc1-ca6ed3c10eee
relation.isOrgUnitOfPublication b3982d12-14ba-4f93-ae05-1abca7e3e557
relation.isOrgUnitOfPublication.latestForDiscovery b3982d12-14ba-4f93-ae05-1abca7e3e557

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