Numerical and Statistical Aerodynamic Performance Analysis of NACA0009 and NACA4415 Airfoils

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dc.authoridEvran, Savas/0000-0002-7512-5997
dc.contributor.authorEvran, Savas
dc.contributor.authorYildir, Salih Zeki
dc.date.accessioned2025-01-27T20:26:55Z
dc.date.available2025-01-27T20:26:55Z
dc.date.issued2024
dc.departmentÇanakkale Onsekiz Mart Üniversitesi
dc.description.abstractIn this numerical and statistical study, lift and drag coefficient performances of NACA-0009 and NACA-4415 airfoils were evaluated in accordance with various attack angle at constant velocity of wind. Lift and drag coefficients of airfoils was numerically determined by computational fluid dynamics code ANSYS FLUENT. Analysis design of numerical calculations was implemented using L16 orthogonal array based on Taguchi method. Angles of attack and airfoil types were considered as control factors. The optimum level and effect of each control factor on responses was statistically implemented using analyses of Signal-to-Noise ratio and variance. As a result of this study, maximum lift and minimum drag coefficient were achieved by using NACA4415 airfoil compared to NACA0009 airfoil. The increase of the angle of attack leads to the increase on the lift and drag coefficients for both airfoils.
dc.description.sponsorshipScientific and Technological Research Council of Turkey [1919B012200301]
dc.description.sponsorshipThe research was supported financially by the Scientific and Technological Research Council of Turkey (TUEBITAK; project application number: 1919B012200301).
dc.identifier.doi10.2339/politeknik.1229081
dc.identifier.issn1302-0900
dc.identifier.issn2147-9429
dc.identifier.issue3
dc.identifier.trdizinid1278770
dc.identifier.urihttps://doi.org/10.2339/politeknik.1229081
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/1278770
dc.identifier.urihttps://hdl.handle.net/20.500.12428/22498
dc.identifier.volume27
dc.identifier.wosWOS:000926819200001
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.publisherGazi Univ
dc.relation.ispartofJournal of Polytechnic-Politeknik Dergisi
dc.relation.publicationcategoryinfo:eu-repo/semantics/openAccess
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_WoS_20250125
dc.subjectAngle of attack
dc.subjectairfoil
dc.subjectCFD
dc.subjectTaguchi method
dc.subjectaerodynamic
dc.titleNumerical and Statistical Aerodynamic Performance Analysis of NACA0009 and NACA4415 Airfoils
dc.typeArticle

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