LEADER 01614nam  2200457I  450 
001 9910704468403321
005 20130701141153.0
035   $a(CKB)5470000002441009
035   $a(OCoLC)851384001
035   $a(EXLCZ)995470000002441009
100   $a20130701d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMethods for assessing honeycomb sandwich panel wrinkling failures / Bart F. Zalewski and William B. Dial, Brett A. Bednarcyk
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (14 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-217697
300   $aTitle from title screen (viewed on July 1, 2013).
300   $a"October 2012."
320   $aIncludes bibliographical references (pages 13-14).
606   $aHoneycomb structures$2nasat
606   $aSandwich structures$2nasat
606   $aFailure modes$2nasat
606   $aFinite element method$2nasat
615  7$aHoneycomb structures.
615  7$aSandwich structures.
615  7$aFailure modes.
615  7$aFinite element method.
700   $aZalewski$b Bartlomiej Francisze$01390011
702   $aDial$b William B.
702   $aBednarcyk$b Brett A.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704468403321
996   $aMethods for assessing honeycomb sandwich panel wrinkling failures$93528203
997   $aUNINA