LEADER 01794nam 2200517 a 450 001 9910699652003321 005 20230902161714.0 035 $a(CKB)5470000002404416 035 $a(OCoLC)704910697 035 $a(EXLCZ)995470000002404416 100 $a20110303d2010 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA critique of a phenomenological fiber breakage model for stress rupture of composite materials$b[electronic resource] /$fJames R. Reeder 210 1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010] 215 $a1 online resource (21 pages) $cillustrations 225 1 $aNASA/TM ;$v2010-216721 300 $aTitle from title screen (viewed on March 3, 2011). 300 $a"July 2010." 320 $aIncludes bibliographical references (page 21) 410 0$aNASA technical memorandum ;$v216721. 606 $aComposite materials$2nasat 606 $aComposite wrapping$2nasat 606 $aFailure modes$2nasat 606 $aLoads (forces)$2nasat 606 $aPressure vessels$2nasat 606 $aProving$2nasat 606 $aComposite structures$2nasat 615 7$aComposite materials. 615 7$aComposite wrapping. 615 7$aFailure modes. 615 7$aLoads (forces) 615 7$aPressure vessels. 615 7$aProving. 615 7$aComposite structures. 700 $aReeder$b James R$01405865 712 02$aLangley Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910699652003321 996 $aA critique of a phenomenological fiber breakage model for stress rupture of composite materials$93545654 997 $aUNINA