dc.contributor.author | Şal, Fırat | |
dc.date.accessioned | 2020-05-24T15:31:54Z | |
dc.date.available | 2020-05-24T15:31:54Z | |
dc.date.issued | 2019 | |
dc.identifier.citation | Şal, F. (2019). Effects of the actively morphing root chord and taper on helicopter energy Aircraft Engineering and Aerospace Technology, 92 (2), pp. 264-270.
https://doi.org/10.1108/AEAT-08-2019-0165 | en_US |
dc.identifier.issn | 1748-8842 | |
dc.identifier.issn | 1758-4213 | |
dc.identifier.uri | https://doi.org/10.1108/AEAT-08-2019-0165 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12508/1151 | |
dc.description | WOS: 000503109600001 | en_US |
dc.description.abstract | Purpose The purpose of this paper presents the effects of actively morphing root chord and taper on the energy of the flight control system (i.e. FCS). Design/methodology/approach Via regarding previously mentioned purposes, sophisticated and realistic helicopter models are benefitted to examine the energy of the FCS. Findings Helicopters having actively morphing blade root chord length and blade taper consume less control energy than the ones having one of or any of passively morphing blade root chord length and blade taper. Practical implications - Actively morphing blade root chord length and blade taper can be used for cheaper helicopter operations. Originality/value The main originality of this paper is applying active morphing strategy on helicopter blade root chord and blade taper. In this paper, it is also found that using active morphing strategy on helicopter blade root chord and blade taper reasons less energy consumption than using either passively morphing blade root chord length plus blade taper or not any. This causes also less fuel consumption and green environment. | en_US |
dc.language.iso | eng | en_US |
dc.publisher | Emerald Group Publishing Ltd | en_US |
dc.relation.isversionof | 10.1108/AEAT-08-2019-0165 | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | Helicopters | 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 energy | en_US |
dc.subject.classification | Sling | Rotary Wing Aircraft | Helicopter | en_US |
dc.subject.classification | Engineering, Aerospace | en_US |
dc.subject.other | Aircraft control | en_US |
dc.subject.other | Energy utilization | en_US |
dc.subject.other | Helicopter services | en_US |
dc.subject.other | Helicopters | en_US |
dc.subject.other | Turbomachine blades | en_US |
dc.subject.other | Blade roots | en_US |
dc.subject.other | Blade taper | en_US |
dc.subject.other | Control energy | en_US |
dc.subject.other | Design/methodology/approach | en_US |
dc.subject.other | Green environments | en_US |
dc.subject.other | Helicopter blades | en_US |
dc.subject.other | Helicopter operation | en_US |
dc.subject.other | Morphing | en_US |
dc.subject.other | Flight control systems | en_US |
dc.subject.other | Vibration Analysis | en_US |
dc.subject.other | Design | en_US |
dc.subject.other | Rotor | en_US |
dc.subject.other | Flight | en_US |
dc.subject.other | Beam | en_US |
dc.title | Effects of the actively morphing root chord and taper on helicopter energy | 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 | 264 | en_US |
dc.identifier.endpage | 270 | 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 |