Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications

Oktay T., Uzun M., Kanat Ö. Ö.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, sa.9, ss.1438-1444, 2018 (SCI-Expanded) identifier identifier

  • 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.