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

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Copy For Citation

Ozgumus O. O., KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.79, no.3, pp.231-237, 2007 (SCI-Expanded)

• Publication Type: Article / Article
• Volume: 79 Issue: 3
• Publication Date: 2007
• Doi Number: 10.1108/00022660710743822
• Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Page Numbers: pp.231-237
• Istanbul Technical University Affiliated: No

Abstract

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