Publication:
Aerodynamic Performance Losses due to Ice Formation on the UAV’s Wings

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cris.virtual.department#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtual.orcid#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtualsource.departmentfd15f02e-3da6-4c2a-aa68-e76494dd6e69
cris.virtualsource.orcidfd15f02e-3da6-4c2a-aa68-e76494dd6e69
dc.contributor.affiliationOsmaniye Korkut Ata Üniversitesi, Osmaniye, Türkiye Türk Hava Kurumu Üniversitesi, Ankara, Türkiye Orta Doğu Teknik Üniversitesi, Ankara, Türkiye
dc.contributor.authorÖzcan YIRTICI Durmuş Sinan KÖRPE Serkan ÖZGEN
dc.date.accessioned2024-07-11T10:49:49Z
dc.date.available2024-07-11T10:49:49Z
dc.date.issued2020
dc.description.abstractIce accretion on unmanned air vehicle’s wing modifies the initial airfoilcontour and changes the aerodynamic characteristic of the wing. The aimof this research is to calculate performance losses on a wing due to theaccretion of rime ice. In this study, ice formation on NREL S826 airfoil ispredicted by using ice accretion tool. The computed aerodynamic loads arecompared for clean wings and iced wings with different aspect ratios. Thecomputations are based on the lifting-line method. According to the results,predicted aerodynamic performance loss is higher for small aspect ratiothan that of the bigger for the rime ice.
dc.description.endpage215
dc.description.issue2
dc.description.startpage207
dc.description.volume13
dc.identifier.eissn2148-1059
dc.identifier.issn1304-0448
dc.identifier.urihttps://acikarsiv.thk.edu.tr/handle/123456789/2058
dc.language.isoeng
dc.relation.journalHavacılık ve Uzay Teknolojileri Dergisi
dc.titleAerodynamic Performance Losses due to Ice Formation on the UAV’s Wings
dc.typeMakale
dc.typeAraştırma Makalesi
dspace.entity.typePublication

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