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, vol.79, no.2, pp.177-183, 2007 (Journal Indexed in SCI) identifier identifier

  • Publication Type: Article / Article
  • Volume: 79 Issue: 2
  • Publication Date: 2007
  • Doi Number: 10.1108/00022660710732734
  • Title of Journal : AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Page Numbers: pp.177-183

Abstract

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.