Computational fluid dynamics-based aerodynamic performance evaluation of naca 64A206 airfoil using ansys fluent

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dc.authorid0009-0002-4286-4352
dc.authorid0000-0002-1723-4108
dc.authorid0000-0002-7672-1846
dc.contributor.authorTaş, Kerem Ali
dc.contributor.authorTanrıver, Kürşat
dc.contributor.authorAy, Mustafa
dc.date.accessioned2026-09-01T14:05:35Z
dc.date.available2026-09-01T14:05:35Z
dc.date.issued2026
dc.departmentFakülteler, Mühendislik ve Doğa Bilimleri Fakültesi, Mekatronik Mühendisliği Bölümü
dc.departmentFakülteler, Mühendislik ve Doğa Bilimleri Fakültesi, Makine Mühendisliği Bölümü
dc.description.abstractAerodynamic performance evaluation of aircraft wings is a critical stage in aircraft design due to its direct influence on lift generation, flight stability, and overall efficiency. Computational Fluid Dynamics (CFD) methods provide an effective approach for predicting flow characteristics around airfoil geometries before experimental testing. Therefore, the objective of this study was to numerically investigate the aerodynamic behavior of the NACA 64A206 airfoil using ANSYS Fluent by evaluating velocity distribution, pressure variation, and lift coefficient characteristics.
dc.identifier.citationTaş, K. A., Tanrıver, K., & Ay, M. (2026). Computational fluid dynamics-based aerodynamic performance evaluation of naca 64A206 airfoil using ansys fluent. 9th International Black Sea Modern Scientific Research Congress, Düzce, Türkiye, (p. 327). Euroasia Journal of Social Sciences & Humanities.
dc.identifier.endpage327
dc.identifier.isbn9798896955177
dc.identifier.startpage327
dc.identifier.urihttps://hdl.handle.net/20.500.13055/1621
dc.institutionauthorTaş, Kerem Ali
dc.institutionauthorTanrıver, Kürşat
dc.institutionauthorAy, Mustafa
dc.institutionauthorid0009-0002-4286-4352
dc.institutionauthorid0000-0002-1723-4108
dc.institutionauthorid0000-0002-7672-1846
dc.language.isoen
dc.publisherEuroasia Journal of Social Sciences & Humanities
dc.relation.ispartof9th International Black Sea Modern Scientific Research Congress
dc.relation.publicationcategoryKonferans Öğesi - Ulusal - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectAircraft Wing
dc.subjectNACA 64A206 Airfoil
dc.subjectComputational Fluid Dynamics
dc.subjectANSYS Fluent
dc.subjectAerodynamic Performance
dc.titleComputational fluid dynamics-based aerodynamic performance evaluation of naca 64A206 airfoil using ansys fluent
dc.typeConference Object
dspace.entity.typePublication

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