Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications
Yazarlar (3)
Prof. Dr. Tuğrul Oktay Erciyes Üniversitesi, Türkiye
Doç. Dr. Metin Uzun Erciyes Üniversitesi, Türkiye
Dr. Öğr. Üyesi Öztürk Özdemir KANAT Kastamonu Üniversitesi, Türkiye
| Makale Türü | Özgün Makale (SSCI, AHCI, SCI, SCI-Exp dergilerinde yayınlanan tam makale) | ||
| Dergi Adı | Aircraft Engineering and Aerospace Technology (Q3) | ||
| Dergi ISSN | 1748-8842 Wos Dergi Scopus Dergi | ||
| Dergi Tarandığı Indeksler | SCI-Expanded | ||
| Makale Dili | İngilizce | Basım Tarihi | 10-2018 |
| Kabul Tarihi | – | Yayınlanma Tarihi | 11-10-2018 |
| Cilt / Sayı / Sayfa | 90 / 9 / 1438–1444 | DOI | 10.1108/AEAT-07-2017-0175 |
| Makale Linki | https://www.emerald.com/insight/content/doi/10.1108/AEAT-07-2017-0175/full/html | ||
| UAK Araştırma Alanları |
Aerodinamik
|
||
| Özet |
| Purpose The purpose of this study is to increase maximum lift/drag ratio (Emax) of tactical unmanned aerial vehicles (TUAVs) via applying novel small aerodynamic modifications. Design methodology/approach A TUAV is manufactured in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory. It has both passive and active morphing capabilities. Its nosecone and tailcone shapes are redesigned to improve Emax. Moreover, active flow control is also built on its wing for improving Emax. Findings Using these novel small aerodynamic modifications, considerable improvement on Emax is obtained. Research limitations/implications Permission of Directorate General of Civil Aviation in Turkey is required for testing TUAVs in real-time applications. Practical implications Small aerodynamic … |
| Anahtar Kelimeler |
| Aerodynamics | Performance improvement | space Maximum lift/drag RATIO | TUAVs |
| Atıf Sayıları | |
| Web of Science | 9 |
| Scopus | 9 |
| Google Scholar | 12 |