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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Atıf İçin Kopyala

Ozgumus O. O., KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.79, sa.3, ss.231-237, 2007 (SCI-Expanded)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 79 Sayı: 3
• Basım Tarihi: 2007
• Doi Numarası: 10.1108/00022660710743822
• Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Sayfa Sayıları: ss.231-237
• İstanbul Teknik Üniversitesi Adresli: Hayır

Özet

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