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, vol.79, no.3, pp.231-237, 2007 (Journal Indexed in SCI) identifier identifier

  • Publication Type: Article / Article
  • Volume: 79 Issue: 3
  • Publication Date: 2007
  • Doi Number: 10.1108/00022660710743822
  • Title of Journal : AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Page Numbers: pp.231-237

Abstract

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