The influence of perturbation motion over a slender delta wing under sideslip angle

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dc.contributor.authorTaşcı, Mehmet Oğuz
dc.contributor.authorTümse, Sergen
dc.contributor.authorŞahin, Beşir
dc.contributor.authorKarasu, İlyas
dc.contributor.authorAkıllı, Hüseyin
dc.date.accessioned2025-01-06T17:23:07Z
dc.date.available2025-01-06T17:23:07Z
dc.date.issued2021
dc.departmentAdana Alparslan Türkeş Bilim ve Teknoloji Üniversitesi
dc.description.abstractIn this study, the main objective is to reveal the change of the vortical flow characteristics on a slender delta wing with a sweep angle of ?=70º under the alteration of three different sideslip angles of ?=0º, 4º, and 8º at three different main angles of attack of ?m=25º, 30º and 35º experimentally. Dye visualization experiments were conducted at a Reynolds number of Re=2x104to analyze qualitatively. The perturbation motion which has amplitudes of ?0=±0.5º and ±1º was applied continuously under the periods of time of Te=0.5s, 1s, and 2s. However, the effects of the low frequency perturbations to which the aircraft is exposed during the maneuver were examined. It is observed that Kelvin-Helmholtz in the case of the perturbed motion vortices is more prominent than static case results of the slender delta wing. The vortex breakdown location on the perturbed delta wing has been changed in a wider range than the static case of the delta wing at zero sideslip angle, ?.
dc.identifier.doi10.28948/ngumuh.780989
dc.identifier.endpage403
dc.identifier.issn2564-6605
dc.identifier.issue1
dc.identifier.startpage393
dc.identifier.trdizinid408392
dc.identifier.urihttps://doi.org/10.28948/ngumuh.780989
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/408392
dc.identifier.urihttps://hdl.handle.net/20.500.14669/641
dc.identifier.volume10
dc.indekslendigikaynakTR-Dizin
dc.language.isoen
dc.relation.ispartofNiğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_20241211
dc.subjectFizik
dc.subjectUygulamalı
dc.subjectMühendislik
dc.subjectMakine
dc.subjectMühendislik
dc.subjectHava ve Uzay
dc.titleThe influence of perturbation motion over a slender delta wing under sideslip angle
dc.typeArticle

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