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

Ozgumus, Özge; KAYA, Metin

doi:10.1108/00022660710732734

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

Atıf İçin Kopyala

Ozgumus O. O., KAYA M. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.79, sa.2, ss.177-183, 2007 (SCI-Expanded)

Yayın Türü: Makale / Tam Makale
Cilt numarası: 79 Sayı: 2
Basım Tarihi: 2007
Doi Numarası: 10.1108/00022660710732734
Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
Sayfa Sayıları: ss.177-183
İstanbul Teknik Üniversitesi Adresli: Hayır

Özet

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.