LEADER 04164nam 22007215 450 001 9910299846603321 005 20250626163847.0 010 $a3-319-04004-9 024 7 $a10.1007/978-3-319-04004-2 035 $a(CKB)3710000000332351 035 $a(EBL)1968278 035 $a(OCoLC)899739229 035 $a(SSID)ssj0001424346 035 $a(PQKBManifestationID)11934317 035 $a(PQKBTitleCode)TC0001424346 035 $a(PQKBWorkID)11366997 035 $a(PQKB)11393838 035 $a(DE-He213)978-3-319-04004-2 035 $a(MiAaPQ)EBC1968278 035 $a(PPN)183521366 035 $a(EXLCZ)993710000000332351 100 $a20150107d2015 u| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aDamage Growth in Aerospace Composites /$fedited by Aniello Riccio 205 $a1st ed. 2015. 210 1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2015. 215 $a1 online resource (278 p.) 225 1 $aSpringer Aerospace Technology,$x1869-1749 300 $aDescription based upon print version of record. 311 08$a3-319-04003-0 320 $aIncludes bibliographical references. 327 $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). 330 $aThis book presents novel methods for the simulation of damage evolution in aerospace composites that will assist in predicting damage onset and growth and thus foster less conservative designs which realize the promised economic benefits of composite materials. The presented integrated numerical/experimental methodologies are capable of taking into account the presence of damage and its evolution in composite structures from the early phases of the design (conceptual design) through to the detailed finite element method analysis and verification phase. The book is based on the GARTEUR Research Project AG-32, which ran from 2007 to 2012, and documents the main results of that project. In addition, the state of the art in European projects on damage evolution in composites is reviewed. While the high specific strength and stiffness of composite materials make them suitable for aerospace structures, their sensitivity to damage means that designing with composites is a challenging task. The new approaches described here will prove invaluable in meeting that challenge. 410 0$aSpringer Aerospace Technology,$x1869-1749 606 $aAerospace engineering 606 $aAstronautics 606 $aCeramic materials 606 $aMechanics, Applied 606 $aSolids 606 $aAerospace Technology and Astronautics 606 $aCeramics 606 $aSolid Mechanics 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aCeramic materials. 615 0$aMechanics, Applied. 615 0$aSolids. 615 14$aAerospace Technology and Astronautics. 615 24$aCeramics. 615 24$aSolid Mechanics. 676 $a620 676 $a620.1 676 $a620.14 676 $a629.1 702 $aRiccio$b Aniello$4edt$4http://id.loc.gov/vocabulary/relators/edt 906 $aBOOK 912 $a9910299846603321 996 $aDamage Growth in Aerospace Composites$91412302 997 $aUNINA