LEADER 01907nam  2200529I  450 
001 9910705295503321
005 20150327155452.0
035   $a(CKB)5470000002448407
035   $a(OCoLC)905726328
035   $a(EXLCZ)995470000002448407
100   $a20150327j201308    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA test for characterizing delamination migration in carbon/epoxy tape laminates /$fJames G. Ratcliffe, Michael W. Czabaj and Thomas K. O'Brien
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 2013.
215   $a1 online resource (19 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218028
300   $aTitle from title screen (viewed March 27, 2015).
300   $a"August 2013."
320   $aIncludes bibliographical references (pages 10-11).
517 3 $aTest for characterizing delamination migration in carbon epoxy tape laminates
606   $aCantilever beams$2nasat
606   $aDelaminating$2nasat
606   $aEpoxy matrix composites$2nasat
606   $aFractography$2nasat
606   $aKinking$2nasat
606   $aFinite element method$2nasat
615  7$aCantilever beams.
615  7$aDelaminating.
615  7$aEpoxy matrix composites.
615  7$aFractography.
615  7$aKinking.
615  7$aFinite element method.
700   $aRatcliffe$b James G.$01397639
702   $aCzabaj$b Michael W.
702   $aO'Brien$b Thomas K.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705295503321
996   $aA test for characterizing delamination migration in carbon$93465742
997   $aUNINA