dc.contributor.author | Şal, Fırat | |
dc.date.accessioned | 2020-05-24T15:31:58Z | |
dc.date.available | 2020-05-24T15:31:58Z | |
dc.date.issued | 2019 | |
dc.identifier.citation | Şal, F. (2019). Analysis of combined passively and actively morphing blade root chord length and blade taper for helicopter control Aircraft Engineering and Aerospace Technology, 92 (2), pp. 172-179. https://doi.org/10.1108/AEAT-04-2019-0077 | en_US |
dc.identifier.issn | 1748-8842 | |
dc.identifier.issn | 1758-4213 | |
dc.identifier.uri | https://doi.org/10.1108/AEAT-04-2019-0077 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12508/1169 | |
dc.description | WOS: 000508436500002 | en_US |
dc.description.abstract | Purpose The purpose of this study is to examine the effect of passive and active morphing of blade root chord length and blade taper on the control effort of the flight control system (FCS) of a helicopter. Design/methodology/approach Physics-based helicopter models, which are functions of passive and active morphing, are created and applied in helicopter FCS design to determine the control effort. Findings Helicopters, having both passively and actively morphing blade root chord length and blade taper, experience less control effort than the ones having either only passively morphing blade root chord length or only blade taper or only actively morphing blade root chord length and blade taper. Originality/value Main novelty of our article is simultaneous application of passive and active morphing ideas on helicopter root chord length and blade taper. It is also proved in this study that using both passive and active morphing ideas on helicopter blade root chord and blade taper causes much less energy consumption than using either only passive morphing idea on helicopter blade root chord and blade taper or only active morphing idea on helicopter blade root chord and blade taper. This also reduces fuel consumption and also makes environment cleaner. | en_US |
dc.language.iso | eng | en_US |
dc.publisher | Emerald Group Publishing Ltd | en_US |
dc.relation.isversionof | 10.1108/AEAT-04-2019-0077 | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | Helicopters | en_US |
dc.subject | Passive morphing | en_US |
dc.subject | Active morphing | en_US |
dc.subject | Blade root chord | en_US |
dc.subject | Blade taper | en_US |
dc.subject | Flight control system | en_US |
dc.subject | Control effort | en_US |
dc.subject.classification | Sling | Rotary Wing Aircraft | Helicopter | en_US |
dc.subject.classification | Engineering, Aerospace | en_US |
dc.subject.other | Energy utilization | en_US |
dc.subject.other | Flight control systems | en_US |
dc.subject.other | Helicopters | en_US |
dc.subject.other | Turbomachine blades | en_US |
dc.subject.other | Autonomous helicopter flights | en_US |
dc.subject.other | Blade roots | en_US |
dc.subject.other | Blade roots | en_US |
dc.subject.other | Control effort | en_US |
dc.subject.other | Control effort | en_US |
dc.subject.other | Helicopter control | en_US |
dc.subject.other | Morphing | en_US |
dc.subject.other | Aircraft control | en_US |
dc.subject.other | Design | en_US |
dc.subject.other | Rotor | en_US |
dc.subject.other | Flight | en_US |
dc.title | Analysis of combined passively and actively morphing blade root chord length and blade taper for helicopter control | en_US |
dc.type | article | en_US |
dc.relation.journal | Aircraft Engineering And Aerospace Technology | en_US |
dc.contributor.department | İskenderun Teknik Üniversitesi | en_US |
dc.contributor.department | Havacılık ve Uzay Bilimleri Fakültesi -- Uçak Bakım ve Onarım Bölümü | en_US |
dc.identifier.volume | 92 | en_US |
dc.identifier.issue | 2 | en_US |
dc.identifier.startpage | 172 | en_US |
dc.identifier.endpage | 179 | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.contributor.isteauthor | Şal, Fırat | en_US |
dc.relation.index | Web of Science Core Collection - Science Citation Index Expanded | en_US |