000 03715nam a22005055i 4500
001 978-3-319-04004-2
003 DE-He213
005 20200421111653.0
007 cr nn 008mamaa
008 150107s2015 gw | s |||| 0|eng d
020 _a9783319040042
_9978-3-319-04004-2
024 7 _a10.1007/978-3-319-04004-2
_2doi
050 4 _aTL787-4050.22
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
082 0 4 _a629.1
_223
245 1 0 _aDamage Growth in Aerospace Composites
_h[electronic resource] /
_cedited by Aniello Riccio.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2015.
300 _aVI, 279 p. 210 illus., 14 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Aerospace Technology,
_x1869-1730
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 _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.
650 0 _aEngineering.
650 0 _aContinuum mechanics.
650 0 _aAerospace engineering.
650 0 _aAstronautics.
650 1 4 _aEngineering.
650 2 4 _aAerospace Technology and Astronautics.
650 2 4 _aCeramics, Glass, Composites, Natural Methods.
650 2 4 _aContinuum Mechanics and Mechanics of Materials.
700 1 _aRiccio, Aniello.
_eeditor.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783319040035
830 0 _aSpringer Aerospace Technology,
_x1869-1730
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-319-04004-2
912 _aZDB-2-ENG
942 _cEBK
999 _c54526
_d54526