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The Rotating Beam Problem in Helicopter Dynamics / by Ranjan Ganguli, Vijay Panchore.

By: Ganguli, Ranjan, autor
Contributor(s): Panchore, Vijay, autor
Material type: materialTypeLabelE-bookSeries: (Foundations of Engineering Mechanics, 1612-1384); (Engineering (Springer-11647)).Publisher: Singapore : Springer International Publishing, 2018Description: 1 recurso en línea (XIII, 99 páginas 46 ilustraciones).ISBN: 9789811060984.Subject: HelicópterosOnline resources: Acceso a este recurso digital (usuarios Universidad Europea de Madrid)Digital Resources
Contents:
Introduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.
Abstract: 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.
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Holdings
Item type Current library Collection Call number Status Date due Barcode Item holds
LIBRO-E NO PRÉSTAMO LIBRO-E NO PRÉSTAMO Madrid Digital Acceso Electrónico (UEM) Ciencias e Ingeniería TL1716 .G364 2018 EB (Browse shelf(Opens below)) Acceso electrónico eBook.15112796
Total holds: 0

Introduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.

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.

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