Aeroelastic behaviour of UAV wings due to morphing

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Unlusoy L., YAMAN Y.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.1, ss.30-38, 2017 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 89 Sayı: 1
  • Basım Tarihi: 2017
  • Doi Numarası: 10.1108/aeat-12-2014-0217
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.30-38
  • Anahtar Kelimeler: Flutter prediction, Morphing wings, Pk-method, State-space solution, Thodorsen aerodynamics, Typical section model, FLUTTER, PREDICTION, DIVERGENCE
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of this paper is to analyse the effects of morphing on the aeroelastic behaviour of unmanned aerial vehicle (UAV) wings to make an emphasis on the required aeroelastic tailoring starting from the conceptual design of the morphing mechanisms.