LEADER 01884nam  2200505I  450 
001 9910706146503321
005 20170906094219.0
035   $a(CKB)5470000002454963
035   $a(OCoLC)1002925933
035   $a(EXLCZ)995470000002454963
100   $a20170906j199908    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects /$fDavid M. McGowan
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 1999.
215   $a1 online resource (x, 97 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209512
300   $a"August 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 59-62).
606   $aPlates (structural members)$2nasat
606   $aBuckling$2nasat
606   $aDesign analysis$2nasat
606   $aDynamic structural analysis$2nasat
606   $aTransverse loads$2nasat
606   $aLoads (forces)$2nasat
606   $aCurves (geometry)$2nasat
615  7$aPlates (structural members)
615  7$aBuckling.
615  7$aDesign analysis.
615  7$aDynamic structural analysis.
615  7$aTransverse loads.
615  7$aLoads (forces)
615  7$aCurves (geometry)
700   $aMcGowan$b David M.$01400479
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706146503321
996   $aDevelopment of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects$93468890
997   $aUNINA