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

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Copy For Citation

Ozgumus O. O., KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.79, no.2, pp.177-183, 2007 (SCI-Expanded)

• Publication Type: Article / Article
• Volume: 79 Issue: 2
• Publication Date: 2007
• Doi Number: 10.1108/00022660710732734
• Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Page Numbers: pp.177-183
• Istanbul Technical University Affiliated: No

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.