Aerodynamic Efficiency Analysis of Variable Morphing Wings

Basit Öğe Kaydı
dc.authorid0000-0003-3319-3657en_US
dc.authorid0000-0001-6818-7682en_US
dc.authorid0000-0002-8028-727Xen_US
dc.contributor.authorKaygan, Erdoğan
dc.contributor.authorKöroğlu, Aslıhan Tuğçe
dc.contributor.authorBaşak, Melisa
dc.date.accessioned2023-08-05T08:20:32Z
dc.date.available2023-08-05T08:20:32Z
dc.date.issued2022 Eylülen_US
dc.departmentBaşka Kurumen_US
dc.description.abstractIn this paper, variable wing and/or winglet concepts are investigated. The impetus for the work was to identify and optimize wing and winglets to enhance the aerodynamic efficiency of a morphing aircraft. The analysis is based on changing sweep angle and wing-tip twist together with cant angle morphing (? = 0° - 45° ? = ?10°- 10° and ? = 0° - 30°). A variety of cases are examined through an aerodynamic analysis tool (VLM) comparing with baseline sweep wing configuration. As a result, significant improvements in flight characteristics are observed by adapting the required angle to receive optimum performance benefits.en_US
dc.identifier.citationKaygan, E., Köroğlu, A. T., Başak, M., (2022). Aerodynamic Efficiency Analysis of Variable Morphing Wings. International Journal of Aeronautics and Astronautics, 3(2), 71-86. DOI: 10.55212/ijaa.1088399en_US
dc.identifier.doi10.55212/ijaa.1088399en_US
dc.identifier.endpage86en_US
dc.identifier.issn2757-6574en_US
dc.identifier.issue2en_US
dc.identifier.startpage71en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12395/49166
dc.identifier.volume3en_US
dc.language.isoenen_US
dc.publisherSelçuk Üniversitesien_US
dc.relation.ispartofInternational Journal of Aeronautics and Astronauticsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Başka Kurum Yazarıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjectAerodynamicsen_US
dc.subjectDragen_US
dc.subjectMorphingen_US
dc.subjectSweepen_US
dc.subjectTwisten_US
dc.titleAerodynamic Efficiency Analysis of Variable Morphing Wingsen_US
dc.typeArticleen_US

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
Küçük Resim
İsim:
ıjaa322.pdf
Boyut:
1.37 MB
Biçim:
Adobe Portable Document Format
Açıklama:
İndir
Lisans paketi
Listeleniyor 1 - 1 / 1
Küçük Resim Yok
İsim:
license.txt
Boyut:
1.44 KB
Biçim:
Item-specific license agreed upon to submission
Açıklama:
İndir

Koleksiyon

Dergi Yayın Koleksiyonu