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035   $a(CKB)5470000002445576
035   $a(OCoLC)870332862
035   $a(EXLCZ)995470000002445576
100   $a20140212d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /$fMichael P. Nemeth
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2013.
215   $a1 online resource (60 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-217999
300   $aTitle from title screen (viewed on Feb. 12, 2014).
300   $a"May 2013."
320   $aIncludes bibliographical references (page 19).
606   $aAnisotropy$2nasat
606   $aAxial compression loads$2nasat
606   $aCylindrical shells$2nasat
606   $aInhomogeneity$2nasat
606   $aLaminates$2nasat
606   $aSandwich structures$2nasat
615  7$aAnisotropy.
615  7$aAxial compression loads.
615  7$aCylindrical shells.
615  7$aInhomogeneity.
615  7$aLaminates.
615  7$aSandwich structures.
700   $aNemeth$b Michael P.$01391721
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704816303321
996   $aAn Approximate solution and master curves for buckling of symmetrically laminated composite cylinders$93514065
997   $aUNINA