LEADER 01968nam  2200493I  450 
001 9910704158703321
005 20160106095059.0
035   $a(CKB)5470000002438077
035   $a(OCoLC)933758756
035   $a(EXLCZ)995470000002438077
100   $a20160106j201508    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels /$fEvan J. Pineda [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dAugust 2015.
215   $a1 online resource (18 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218861
300   $aTitle from title screen (viewed on Jan. 6, 2016).
300   $a"August 2015."
300   $a"Prepared for the 30th Annual Technical Conference sponsored by the American Society for Composites, East Lansing, Michigan, September 28-30, 2015."
300   $a"Paper no. 1713."
320   $aIncludes bibliographical references (pages 16-18).
606   $aSpacecraft shielding$2nasat
606   $aCurved panels$2nasat
606   $aHoneycomb cores$2nasat
606   $aDebonding (materials)$2nasat
606   $aHeavy lift launch vehicles$2nasat
615  7$aSpacecraft shielding.
615  7$aCurved panels.
615  7$aHoneycomb cores.
615  7$aDebonding (materials)
615  7$aHeavy lift launch vehicles.
700   $aPineda$b Evan J.$01387412
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704158703321
996   $aA numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels$93459422
997   $aUNINA