LEADER 01824nam  2200481I  450 
001 9910705251603321
005 20141212150656.0
035   $a(CKB)5470000002448851
035   $a(OCoLC)898081538
035   $a(EXLCZ)995470000002448851
100   $a20141212j201307    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFloating node method and virtual crack closure techique for modeling matrix cracking-delamination interaction /$fN.V. De Carvalho [and five others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 2013.
215   $a1 online resource (17 pages) $ccolor illustrations
225 1 $aNASA-CR ;$v2013-218022
300   $aTitle from title screen (viewed Dec. 12, 2014).
300   $a"July 2013."
320   $aIncludes bibliographical references (page 11).
517 3 $aFloating node method and virtual crack closure technique for modeling matrix cracking delamination interaction
606   $aCrack closure$2nasat
606   $aFracture mechanics$2nasat
606   $aDelaminating$2nasat
606   $aPly orientation$2nasat
606   $aLaminates$2nasat
615  7$aCrack closure.
615  7$aFracture mechanics.
615  7$aDelaminating.
615  7$aPly orientation.
615  7$aLaminates.
700   $aDe Carvalho$b N. V.$01414748
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705251603321
996   $aFloating node method and virtual crack closure techique for modeling matrix cracking-delamination interaction$93514893
997   $aUNINA