000			03446nam a22004935i 4500
001			978-1-4020-4203-4
003			DE-He213
005			20251006084506.0
007			cr nn 008mamaa
008			100301s2006 ne | s |||| 0|eng d
020			_a9781402042034
020			_a99781402042034
024	7		_a10.1007/1-4020-4203-5 _2doi
082	0	4	_a620 _223
100	1		_aLibrescu, Liviu. _eauthor.
245	1	0	_aThin-Walled Composite Beams _h[electronic resource] : _bTheory and Application / _cby Liviu Librescu, Ohseop Song.
264		1	_aDordrecht : _bSpringer Netherlands, _c2006.
300			_aXXVI, 607 p. _bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	1		_aSolid Mechanics and Its Applications, _x0925-0042 ; _v131
505	0		_aKinematics of Thin Walled Beams -- The Equations of Motion of Open/Closed Cross-Section Beams -- Additional Equations of the Linear Beam Theory -- Several Theorems in Linear Thin-Walled Beam Theory -- Free Vibration -- Dynamic Response to Time-Dependent External Excitation -- Thin-Walled Beams Carrying Stores -- Rotating Thin-Walled Anisotropic Beams -- Spinning Thin-Walled Anisotropic Beams -- Thermally Induced Vibration and Control of Spacecraft Booms -- Aeroelasticity of Thin-Walled Aircraft Wings -- Open-Section Beams.
520			_aThis is the first monograph devoted to the foundation of the theory of composite anisotropic thin-walled beams and to its applications in various problems involving the aeronautical/aerospace, helicopter, naval and mechanical structures. Throughout the theoretical part, an effort was made to provide the treatment of the subject by using the equations of the 3-D elasticity theory. Non-classical effects such as transverse shear, warping constraint, anisotropy of constituent materials yielding the coupling of twist-bending (lateral), bending (transversal)-extension have been included and their implications have been thoroughly analyzed. Thermal effects have been included and in order to be able to circumvent their deleterious effects, functionally graded materials have been considered in their construction. Implications of the application of the tailoring technique and of the active feedback control on free vibration, dynamic response, instability and aeroelasticity of such structures have been amply investigated. Special care was exercised throughout this work to address and validate the adopted solution methodologies and the obtained results against those available in the literature and obtained via numerical or experimental means.
650		0	_aENGINEERING.
650		0	_aMECHANICS, APPLIED.
650		0	_aMECHANICAL ENGINEERING.
650		0	_aVIBRATION.
650	1	4	_aENGINEERING.
650	2	4	_aENGINEERING, GENERAL.
650	2	4	_aTHEORETICAL AND APPLIED MECHANICS.
650	2	4	_aSTRUCTURAL MECHANICS.
650	2	4	_aVIBRATION, DYNAMICAL SYSTEMS, CONTROL.
700	1		_aSong, Ohseop. _eauthor.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9781402034572
830		0	_aSolid Mechanics and Its Applications, _x0925-0042 ; _v131
856	4	0	_uhttp://dx.doi.org/10.1007/1-4020-4203-5 _zVer el texto completo en las instalaciones del CICY
912			_aZDB-2-ENG
942			_2ddc _cER
999			_c60772 _d60772