Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I


Ozgumus O. O. , KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.79, ss.177-183, 2007 (SCI İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 79 Konu: 2
  • Basım Tarihi: 2007
  • Doi Numarası: 10.1108/00022660710732734
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.177-183

Özet

Purpose - This study aims to derive the kinetic and the potential energy expressions of a rotating uniform hingeless rotor blade and the aerodynamic loads that act on the blade element in hovering flight conditions.