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100   $a20130526j199702    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDamage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets /$fDavid M. McGowan and Damodar R. Ambur
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 1997.
215   $a1 online resource (37 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110303
300   $a"February 1997."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 12-13).
606   $aGraphite-epoxy composites$2nasat
606   $aHoneycomb cores$2nasat
606   $aImpact damage$2nasat
606   $aNotch sensitivity$2nasat
606   $aSandwich structures$2nasat
615  7$aGraphite-epoxy composites.
615  7$aHoneycomb cores.
615  7$aImpact damage.
615  7$aNotch sensitivity.
615  7$aSandwich structures.
700   $aMcGowan$b David M.$01400479
702   $aAmbur$b Damodar R.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707910503321
996   $aDamage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets$93467456
997   $aUNINA