The Rotating Beam Problem in Helicopter Dynamics

Vijay Panchore, Ranjan Ganguli

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Springer Singapore img Link Publisher

Naturwissenschaften, Medizin, Informatik, Technik / Maschinenbau, Fertigungstechnik

Beschreibung

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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Schlagwörter

fluid- and aerodynamics, Helicopter flapping blade, Computational method, Finite element method in time, Aeroelastic stability, Finite element method in space