000			03325nam a22003855i 4500
001			84567
003			ES-MaUEC
005			20230207040430.0
007			cr nn 008mamaa
008			160206s2016 gw | s |||| 0|eng d
020			_a9783319149592
040			_aES-MaUEC
050		4	_aTA664 _b.G467 2016
082	0	4	_a620.1
100	1		_aGhorashi, Mehrdaad _0Local _996840
245	1	0	_aStatics and Rotational Dynamics of Composite Beams _cby Mehrdaad Ghorashi
250			_a1st ed.
260			_aCham _bSpringer International Publishing _c2016
300			_a1 recurso en línea (XIX, 227 páginas) _b148 ilustraciones, 25 ilustraciones en color
336			_aTexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
505	0		_aIntroduction -- Review of the Variational Asymptotic Method and the Intrinsic Equations of a Beam -- Linear Static Analysis of Composite Beams -- Nonlinear Static Analysis of Composite Beams -- Transient Nonlinear Dynamics of Accelerating Hingeless Rotating Blades -- Steady State and Perturbed Steady-State Nonlinear Dynamics of Hingeless Rotating Blades -- Rigid and Elastic Articulated Rotating Composite Blades -- Static and Dynamic Analysis of Beams with Embedded Anisotropic Piezocomposite -- Appendices. .
520	3		_aThis book presents a comprehensive study of the nonlinear statics and dynamics of composite beams and consists of solutions with and without active elements embedded in the beams. The static solution provides the initial conditions for the dynamic analysis. The dynamic problems considered include the analyses of clamped (hingeless) and articulated (hinged) accelerating rotating beams. Two independent numerical solutions for the steady state and the transient responses are presented. The author illustrates that the transient solution of the nonlinear formulation of accelerating rotating beam converges to the steady state solution obtained by the shooting method. Other key areas considered include calculation of the effect of perturbing the steady state solution, coupled nonlinear flap-lag dynamics of a rotating articulated beam with hinge offset and aerodynamic damping, and static and dynamic responses of nonlinear composite beams with embedded anisotropic piezo-composite actuators. The book is intended as a thorough study of nonlinear elasticity of slender beams and is targeted to researchers, graduate students, and practicing engineers in the fields of structural dynamics, aerospace structures, and mechanical engineering.
710	2		_aSpringerLink (Online service) _0Local _9106996
942			_2lcc _cLE
988			_aEBOOK, asignarmaterias , EBSPRINGER
650	0	7	_aAnálisis estructural (Ingeniería) _0 _2embne _9150495
650		7	_aAnálisis estructural (Ingeniería) _0(OCoLC)1135602 _2embne _0 _9150495
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://link.springer.com/book/10.1007/978-3-319-14959-2 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
901			_ai9783319149592
907			_a.b12938452 _b10-10-17 _c21-11-16
998			_am _a_alco _a_vill _b - - _cm _dz _e- _feng _ggw _h0
945			_aTA664 .G467 2016 EB _g1 _ieBOOK _j0 _lmae _o- _pEUR0.00 _q- _r- _sb _t15 _u0 _v0 _w0 _x0 _y.i11583034 _z06-04-17
999			_c84567 _d84567 _x1