000			03538nam a22003855i 4500
999			_c103595 _d103595 _x1
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005			20230102113137.0
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007			cr nn 008mamaa
008			150107s2015 gw | s |||| 0|eng d
020			_a9783319040042
024	7		_a10.1007/978-3-319-04004-2 _2doi
040			_bspa _dES-MaUEC
050		4	_aTA418.9.C6 _bD363 2015 EB
245	1	0	_aDamage Growth in Aerospace Composites _cedited by Aniello Riccio.
264		1	_aCham _bSpringer International Publishing _c2015
300			_a1 recurso en línea (VI, 279 páginas 210 ilustraciones, 14 ilustraciones a color.)
336			_2rdacontent _aTexto (visual) _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
490	0		_aSpringer Aerospace Technology, _x1869-1730
490	0		_aEngineering (Springer-11647)
505	0		_aIntroduction -- Detailed methodologies for integrated delamination growth and fiber-matrix damage progression simulation -- Delamination Growth in Composite Plates under Fatigue Loading Conditions -- Influence of intralaminar damage on the delamination crack evolution -- Microdamage modeling in laminates -- Finite element study of delaminations in notched composites -- Effect of the damage extension through the thickness on the calculation of the residual strength of impacted composite laminates -- A Fast Numerical Methodology for Delamination Growth Initiation Simulation -- An Experimental Study on the strength of out of plane loaded composite structures -- Buckling and collapse tests using advanced measurement systems -- Vacuum infusion manufacturing of CFRP panels with induced delamination -- Lock-in Thermography to detect delamination in Carbon Fibers Reinforced Polymers (Carosena Meola and Giovanni M. Carlomagno).
520	3		_aThis book presents novel methods for the simulation of damage evolution in aerospace composites that will assist in predicting damage onset and growth and thus foster less conservative designs which realize the promised economic benefits of composite materials. The presented integrated numerical/experimental methodologies are capable of taking into account the presence of damage and its evolution in composite structures from the early phases of the design (conceptual design) through to the detailed finite element method analysis and verification phase. The book is based on the GARTEUR Research Project AG-32, which ran from 2007 to 2012, and documents the main results of that project. In addition, the state of the art in European projects on damage evolution in composites is reviewed. While the high specific strength and stiffness of composite materials make them suitable for aerospace structures, their sensitivity to damage means that designing with composites is a challenging task. The new approaches described here will prove invaluable in meeting that challenge.
988			_aEBSPRINGER_2018
650		7	_aMateriales compuestos _2embne _9141674
700	1		_aRiccio, Aniello. _eeditor literario _4edt _4http://id.loc.gov/vocabulary/relators/edt _1http://viaf.org/viaf/96205511/
776	0	8	_iEdición impresa: _z9783319040035
776	0	8	_iEdición impresa: _z9783319040059
776	0	8	_iEdición impresa: _z9783319381633
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-319-04004-2 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b03/2019 _dz _eIG _zSI