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The rotating beam problem in helicop...

Ganguli, Ranjan.

The rotating beam problem in helicopter dynamics

Record Type:	Electronic resources : Monograph/item
Title/Author:	The rotating beam problem in helicopter dynamicsby Ranjan Ganguli, Vijay Panchore.
Author:	Ganguli, Ranjan.
other author:	Panchore, Vijay.
Published:	Singapore :Springer Singapore :2018.
Description:	xiii, 99 p. :ill., digital ;24 cm.
Contained By:	Springer eBooks
Subject:	Rotational motion (Rigid dynamics)
Online resource:	http://dx.doi.org/10.1007/978-981-10-6098-4
ISBN:	9789811060984$q(electronic bk.)

The rotating beam problem in helicopter dynamics
Ganguli, Ranjan.

The rotating beam problem in helicopter dynamics[electronic resource] /by Ranjan Ganguli, Vijay Panchore. - Singapore :Springer Singapore :2018. - xiii, 99 p. :ill., digital ;24 cm. - Foundations of engineering mechanics,1612-1384. - Foundations of engineering mechanics..

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.

ISBN: 9789811060984$q(electronic bk.)

Standard No.: 10.1007/978-981-10-6098-4doiSubjects--Topical Terms:

743451
Rotational motion (Rigid dynamics)

LC Class. No.: TL1716 / .G35 2017

Dewey Class. No.: 629.13436

The rotating beam problem in helicopter dynamics
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245 1 4 $a The rotating beam problem in helicopter dynamics $h [electronic resource] / $c by Ranjan Ganguli, Vijay Panchore.
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300 $a xiii, 99 p. : $b ill., digital ; $c 24 cm.
490 1 $a Foundations of engineering mechanics, $x 1612-1384
505 0 $a Introduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.
520 $a 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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650 2 4 $a Theoretical and Applied Mechanics. $3 274501
650 2 4 $a Fluid- and Aerodynamics. $3 376797
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
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