LEADER 02516oam 2200661I 450 001 9910708661003321 005 20170405152542.0 035 $a(CKB)5470000002470615 035 $a(OCoLC)844605587 035 $a(EXLCZ)995470000002470615 100 $a20130526j199704 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFatigue debonding characterization in composite skin/stringer configurations /$fMichael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center ;$aAlexandria, Virginia :$cU.S. Army Materiel Command,$dApril 1997. 215 $a1 online resource (33 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v110331 225 1 $aU. S. Army Research Laboratory technical report ;$vARL-TR-1342 300 $a"April 1997." 300 $aTechnical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa. 300 $a"Performing organization: NASA Langley Research Center" Report documentation page. 320 $aIncludes bibliographical references (page 12). 606 $aFatigue tests$2nasat 606 $aDebonding (materials)$2nasat 606 $aComposite structures$2nasat 606 $aFlanges$2nasat 606 $aSkin (structural member)$2nasat 606 $aBonded joints$2nasat 606 $aCrack initiation$2nasat 606 $aDelaminating$2nasat 606 $aGraphite-epoxy composites$2nasat 606 $aResin matrix composites$2nasat 615 7$aFatigue tests. 615 7$aDebonding (materials) 615 7$aComposite structures. 615 7$aFlanges. 615 7$aSkin (structural member) 615 7$aBonded joints. 615 7$aCrack initiation. 615 7$aDelaminating. 615 7$aGraphite-epoxy composites. 615 7$aResin matrix composites. 700 $aCvitkovich$b Michael$01423002 702 $aO'Brien$b T. Kevin 702 $aMinguet$b Pierre Jacques 712 02$aUnited States.$bArmy Materiel Command. 712 02$aLangley Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910708661003321 996 $aFatigue debonding characterization in composite skin$93549062 997 $aUNINA