Investigation of the effective factors on solar powered fixed-wing UAV for extended flight endurance

Basit Öğe Kaydı
dc.contributor.authorAlfalari, Aws
dc.contributor.authorAlaiwi, Yaser
dc.date.accessioned2022-12-27T16:46:55Z
dc.date.available2022-12-27T16:46:55Z
dc.date.issued2022en_US
dc.departmentEnstitüler, Lisansüstü Eğitim Enstitüsü, Makine Mühendisliği Ana Bilim Dalıen_US
dc.description.abstractIn recent years, big interest of wing geometry emerged because it affects all other aircraft components. Geometry affects aircraft forces due to airflow characteristics. Solar cells enhance the plane's flying time. This research examines how wing designs affect airfoil characteristics. This simulation was done using CFD ANSYS analysis. These two varieties were chosen to better understand the forces on subsonic aircraft and enhance the wing shape design. In this investigation, air speed was (5.5, 8.8, and 11.11 m/s). CFD Simulation shows that the two kinds of airfoils have similar lift and drag coefficients were determined according to angle of attack. The lift coefficient and drag coefficient were determined according to air speed. In both cases, angle of attack was increased gradually. When the attack angle increases, drag force increases too. Drag generated a downwash of air behind the wing, threatening lift and stability. Current work employs optimum wing design to avoid this problem. The revised proposed wing reduces induced drag by separating top and bottom loads. The investigation lengthened the plane's flight and reduced its power. Lift force, lift coefficient, and drag coefficient affect wing performance.en_US
dc.identifier.citationAlfalari, A., Alaiwi, Y. (2022). Investigation of the effective factors on solar powered fixed-wing UAV for extended flight endurance. In 2022 International Symposium on Multidisciplinary Studies and Innovative Technologies (ISMSIT) (pp. 828-833). IEEE.en_US
dc.identifier.endpage833en_US
dc.identifier.isbn9781665470131
dc.identifier.scopus2-s2.0-85142796209
dc.identifier.scopusqualityN/A
dc.identifier.startpage828en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12939/3157
dc.indekslendigikaynakScopus
dc.institutionauthorAlfalari, Aws
dc.institutionauthorAlaiwi, Yaser
dc.language.isoen
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.relation.ispartofISMSIT 2022 - 6th International Symposium on Multidisciplinary Studies and Innovative Technologies, Proceedings
dc.relation.isversionof10.1109/ISMSIT56059.2022.9932721en_US
dc.relation.publicationcategoryKonferans Öğesi - Ulusal - İdari Personel ve Öğrencien_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectS1223en_US
dc.subjectS1223RTLen_US
dc.subjectUAVen_US
dc.subjectWing Performanceen_US
dc.titleInvestigation of the effective factors on solar powered fixed-wing UAV for extended flight endurance
dc.typeConference Object

Dosyalar

Lisans paketi
Listeleniyor 1 - 1 / 1
[ X ]
Ä°sim:
license.txt
Boyut:
1.44 KB
Biçim:
Item-specific license agreed upon to submission
Açıklama:
Ä°ndir

Koleksiyon

Scopus İndeksli Yayınlar Koleksiyonu