LEADER 01606nam  2200445I  450 
001 9910706250303321
005 20171018073201.0
035   $a(CKB)5470000002455934
035   $a(OCoLC)1006582786
035   $a(EXLCZ)995470000002455934
100   $a20171018j201708    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aConstitutive modeling of the facesheet to core interface in honeycomb sandwich panels subject to mode I delamination / Daniel Ho?wer [and five others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dAugust 2017.
215   $a1 online resource (44 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219470
300   $a"August 2017."
320   $aIncludes bibliographical references (pages 39-44).
606   $aCarbon fibers$2nasat
606   $aDelaminating$2nasat
606   $aFinite element method$2nasat
606   $aHoneycomb structures$2nasat
606   $aSandwich structures$2nasat
615  7$aCarbon fibers.
615  7$aDelaminating.
615  7$aFinite element method.
615  7$aHoneycomb structures.
615  7$aSandwich structures.
700   $aHo?wer$b Daniel$01413659
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706250303321
996   $aConstitutive modeling of the facesheet to core interface in honeycomb sandwich panels subject to mode I delamination$93510566
997   $aUNINA