Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover

Ozgumus O. O. , KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.79, sa.3, ss.231-237, 2007 (SCI İndekslerine Giren Dergi) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 79 Konu: 3
  • Basım Tarihi: 2007
  • Doi Numarası: 10.1108/00022660710743822
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.231-237

Özet

Purpose - This study aims to carry out flutter stability and vibration analysis of a uniform hingeless rotor blade in hovering flight conditions.