LEADER 01609nam  2200457I  450 
001 9910705740703321
005 20170627115705.0
035   $a(CKB)5470000002453001
035   $a(OCoLC)991868937
035   $a(EXLCZ)995470000002453001
100   $a20170627j201606    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 03$aAn enriched shell finite element for progressive damage simulation in composite laminates /$fMark W. McElroy
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 2016.
215   $a1 online resource (53 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2016-219211
300   $a"June 2016."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 46-53).
606   $aComposite materials$2nasat
606   $aComposite structures$2nasat
606   $aCrack closure$2nasat
606   $aDelaminating$2nasat
606   $aLaminates$2nasat
615  7$aComposite materials.
615  7$aComposite structures.
615  7$aCrack closure.
615  7$aDelaminating.
615  7$aLaminates.
700   $aMcElroy$b Mark W.$01127364
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705740703321
996   $aAn enriched shell finite element for progressive damage simulation in composite laminates$93462445
997   $aUNINA