The Rotating Beam Problem in Helicopter Dynamics (Hardcover, 1st ed. 2018)

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.

General

Imprint:	Springer Verlag, Singapore
Country of origin:	Singapore
Series:	Foundations of Engineering Mechanics
Release date:	October 2017
First published:	2018
Authors:	Ranjan Ganguli • Vijay Panchore
Dimensions:	235 x 155mm (L x W)
Format:	Hardcover
Pages:	99
Edition:	1st ed. 2018
ISBN-13:	978-981-10-6097-7
Categories:	Books > Science & Mathematics > Physics > Classical mechanics > Fluid mechanics Books > Professional & Technical > Transport technology > Aerospace & aviation technology > General Books > Professional & Technical > Mechanical engineering & materials > Materials science > Mechanics of solids > General
LSN:	981-10-6097-5
Barcode:	9789811060977

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