Flight flutter testing and aeroelastic stability of aircraft

Kayran A.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.79, sa.5, ss.494-506, 2007 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 79 Sayı: 5
  • Basım Tarihi: 2007
  • Doi Numarası: 10.1108/00022660710780623
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.494-506
  • Anahtar Kelimeler: aerodynamics, flight dynamics, aircraft, PREDICTION
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

Purpose - This paper sets out to provide a general review of the flight flutter test techniques utilized in aeroelastic stability flight testing of aircraft, and to highlight the key items involved in flight flutter testing of aircraft, by emphasizing all the main information processed during the flutter stability verification based on flight test data.