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The rotating beam problem in helicop...

Ganguli, Ranjan.

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The rotating beam problem in helicopter dynamics

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	The rotating beam problem in helicopter dynamics/ by Ranjan Ganguli, Vijay Panchore.
作者:	Ganguli, Ranjan.
其他作者:	Panchore, Vijay.
出版者:	Singapore :Springer Singapore : : 2018.,
面頁冊數:	xiii, 99 p. :ill., digital ;24 cm.
內容註:	Introduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.
Contained By:	Springer eBooks
標題:	Rotational motion (Rigid dynamics) -
電子資源:	http://dx.doi.org/10.1007/978-981-10-6098-4
ISBN:	9789811060984

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

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

2188895
Rotational motion (Rigid dynamics)

LC Class. No.: TL1716 / .G35 2017

Dewey Class. No.: 629.13436

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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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