000			02196nam a22003255i 4500
001			102824
003			DE-He213
005			20230102113101.0
007			cr nn 008mamaa
008			171014s2018 si | s |||| 0|eng d
020			_a9789811060984
024	7		_a10.1007/978-981-10-6098-4 _2doi
050		4	_aTL716 _b.G364 2018 EB
100	1		_aGanguli, Ranjan _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _0http://id.loc.gov/authorities/names/nb2011022695 _1http://viaf.org/viaf/285499977/ _997725
245	1	4	_aThe Rotating Beam Problem in Helicopter Dynamics _cby Ranjan Ganguli, Vijay Panchore.
264		1	_aSingapore _bSpringer International Publishing _c2018
300			_a1 recurso en línea (XIII, 99 páginas 46 ilustraciones)
347			_atext file _bPDF
490	0		_aFoundations of Engineering Mechanics _x1612-1384
505	0		_aIntroduction -- Finite element analysis in space -- Finite element in time -- Stability analysis -- Helicopter rotor results.
520	3		_aThe 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.
650		7	_aHelicópteros _2embne _9667207
700	1		_aPanchore, Vijay _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut
776	0	8	_iEdición impresa: _z9789811060977
776	0	8	_iEdición impresa: _z9789811060991
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-10-6098-4 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
490	0		_aEngineering (Springer-11647)
988			_aEBSPRINGER_2018
998			_b01/2019 _dz _ea _feng _ggw _h0
999			_c102824 _d102824 _x1