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 (SCI-Expanded) identifier identifier

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.