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The Rotating Beam Problem in Helicopter Dynamics [electronic resource] / by Ranjan Ganguli, Vijay Panchore.

By: Ganguli, Ranjan [author.].
Contributor(s): Panchore, Vijay [author.] | SpringerLink (Online service).
Material type: materialTypeLabelBookSeries: Foundations of Engineering Mechanics: Publisher: Singapore : Springer Nature Singapore : Imprint: Springer, 2018Edition: 1st ed. 2018.Description: XIII, 99 p. 46 illus. online resource.Content type: text Media type: computer Carrier type: online resourceISBN: 9789811060984.Subject(s): Mechanics, Applied | Continuum mechanics | Aerospace engineering | Astronautics | Engineering Mechanics | Continuum Mechanics | Aerospace Technology and AstronauticsAdditional physical formats: Printed edition:: No title; Printed edition:: No title; Printed edition:: No titleDDC classification: 620.1 Online resources: Click here to access online
Contents:
Introduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.
In: Springer Nature eBookSummary: 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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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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