Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, sa.9, ss.1438-1444, 2018 (SCI-Expanded, Scopus)
- Yayın Türü: Makale / Tam Makale
- Cilt numarası: 90 Sayı: 9
- Basım Tarihi: 2018
- Doi Numarası: 10.1108/aeat-07-2017-0175
- Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
- Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
- Sayfa Sayıları: ss.1438-1444
- Anahtar Kelimeler: Performance improvement, Aerodynamics, space Maximum lift, drag RATIO, TUAVs
- Erciyes Üniversitesi Adresli: Evet
Özet
Purpose - The purpose of this study is to increase maximum lift/drag ratio (E-max) of tactical unmanned aerial vehicles (TUAVs) via applying novel small aerodynamic modifications.