000			02954nam a22005175i 4500
001			978-0-387-75591-5
003			DE-He213
005			20140220084455.0
007			cr nn 008mamaa
008			100301s2010 xxu| s |||| 0|eng d
020			_a9780387755915 _9978-0-387-75591-5
024	7		_a10.1007/978-0-387-75591-5 _2doi
050		4	_aTA355
050		4	_aTA352-356
072		7	_aTGMD4 _2bicssc
072		7	_aTEC009070 _2bisacsh
072		7	_aSCI018000 _2bisacsh
082	0	4	_a620 _223
100	1		_aHamidzadeh, Hamid R. _eauthor.
245	1	0	_aVibrations of Thick Cylindrical Structures _h[electronic resource] / _cby Hamid R. Hamidzadeh, Reza N. Jazar.
264		1	_aBoston, MA : _bSpringer US, _c2010.
300			_bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
505	0		_aGoverning Equations -- Vibration of Single-Layer Cylinder -- Modal Analysis of Cylindrical Structures -- Vibration of Multi-Layer thick cylinders -- Constrained Layer Damping Treatment of Thick Cylindrical Structures -- Vibrations of Partial Cylindrical Panels.
520			_aDue to strong potential applications and more demanding requirements imposed on long and thick cylindrical structures, there has been increased research and development activities during recent years in the field of vibration and passive vibration control. An important step in the study of cylindrical structures is the determination of their vibration modal characteristics. This modal information plays a key role in the design and vibration suppression of these structures when subjected to dynamic excitations. Most reported studies on the dynamic response of cylindrical structures have been restricted to the application of the shell theories. These theories are based on a number of simplifying assumptions. The most important of which is, the considered shell must be relatively thin to assume constant stresses within the cylinder. Therefore, due to this limitation, shell theories are inadequate to accurately describe all possible vibration modes in thick cylindrical structures. Vibrations of Thick Cylindrical Structures addresses these problems by applying the theory of elasto-dynamics.
650		0	_aEngineering.
650		0	_aMechanics.
650		0	_aMechanics, applied.
650		0	_aVibration.
650		0	_aMechanical engineering.
650	1	4	_aEngineering.
650	2	4	_aVibration, Dynamical Systems, Control.
650	2	4	_aTheoretical and Applied Mechanics.
650	2	4	_aMechanical Engineering.
650	2	4	_aMechanics.
700	1		_aJazar, Reza N. _eauthor.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9780387755908
856	4	0	_uhttp://dx.doi.org/10.1007/978-0-387-75591-5
912			_aZDB-2-ENG
999			_c109789 _d109789