01609nam 2200457I 450 991070574070332120170627115705.0(CKB)5470000002453001(OCoLC)991868937(EXLCZ)99547000000245300120170627j201606 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAn enriched shell finite element for progressive damage simulation in composite laminates /Mark W. McElroyHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,June 2016.1 online resource (53 pages) color illustrationsNASA/TP ;2016-219211"June 2016.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 46-53).Composite materialsnasatComposite structuresnasatCrack closurenasatDelaminatingnasatLaminatesnasatComposite materials.Composite structures.Crack closure.Delaminating.Laminates.McElroy Mark W.1127364Langley Research Center,GPOGPOBOOK9910705740703321An enriched shell finite element for progressive damage simulation in composite laminates3462445UNINA