The Rotating Beam Problem in Helicopter Dynamics

The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time doma...

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Detaylı Bibliyografya
Asıl Yazarlar: Ganguli, Ranjan (Yazar), Panchore, Vijay (Yazar)
Müşterek Yazar: SpringerLink (Online service)
Materyal Türü: e-Kitap
Dil:İngilizce
Baskı/Yayın Bilgisi: Singapore : Springer Nature Singapore : 2018.
Imprint: Springer,
Edisyon:1st ed. 2018.
Seri Bilgileri:Foundations of Engineering Mechanics,
Konular:
Mechanics, Applied.
Continuum mechanics.
Aerospace engineering.
Astronautics.
Engineering Mechanics.
Continuum Mechanics.
Aerospace Technology and Astronautics.
Online Erişim:Full-text access
Diğer Bilgiler
Özet:The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time domain for the free vibration, aeroelastic response and stability problems. The use of Floquet analysis for the aeroelastic stability analysis of rotor blades is also shown. The contents of the book will be useful to researchers in aerodynamics and applied mechanics, and will also serve well professionals working in the aerospace industry.
Fiziksel Özellikler:XIII, 99 p. 46 illus. online resource.
ISBN:9789811060984
ISSN:1860-6237
DOI:10.1007/978-981-10-6098-4

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