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035   $a(CKB)5470000002430851
035   $a(OCoLC)904125145
035   $a(EXLCZ)995470000002430851
100   $a20150227j201403    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBuckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory /$fMichael P. Nemeth
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMarch 2014.
215   $a1 online resource (408 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218176
300   $aTitle from title screen (viewed Feb. 27, 2015).
300   $a"March 2014."
320   $aIncludes bibliographical references (pages 131-138).
606   $aNonlinear equations$2nasat
606   $aRayleigh-Ritz method$2nasat
606   $aShell theory$2nasat
606   $aShell stability$2nasat
606   $aAnisotropic shells$2nasat
606   $aDonnell equations$2nasat
615  7$aNonlinear equations.
615  7$aRayleigh-Ritz method.
615  7$aShell theory.
615  7$aShell stability.
615  7$aAnisotropic shells.
615  7$aDonnell equations.
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   $a9910702735003321
996   $aBuckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory$93481438
997   $aUNINA