LEADER 02881oam 2200853 450 001 9910705251203321 005 20210820074229.0 035 $a(CKB)5470000002448855 035 $a(OCoLC)889078029 035 $a(EXLCZ)995470000002448855 100 $a20140825g20132014 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aBuckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel /$fDavid E. Myers, Evan J. Pineda [and four others] 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2013-2014. 215 $a1 online resource (3 volumes) $ccolor illustrations 225 1 $aNASA/TM ;$v2013-217822 225 1 $aNASA/TM ;$v2014-217822 320 $aIncludes bibliographical references. 327 $apt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets. 606 $aFibrous composites 606 $aFinite element method 606 $aHoneycomb structures 606 $aFibrous composites$2fast 606 $aFinite element method$2fast 606 $aHoneycomb structures$2fast 606 $aAres 5 cargo launch vehicle$2nasat 606 $aEpoxy matrix composites$2nasat 606 $aFiber composites$2nasat 606 $aFinite element method$2nasat 606 $aHoneycomb structures$2nasat 606 $aRobustness (mathematics)$2nasat 606 $aSandwich structures$2nasat 608 $aTechnical reports.$2fast 608 $aEbook. 608 $aTechnical reports.$2lcgft 615 0$aFibrous composites. 615 0$aFinite element method. 615 0$aHoneycomb structures. 615 7$aFibrous composites. 615 7$aFinite element method. 615 7$aHoneycomb structures. 615 7$aAres 5 cargo launch vehicle. 615 7$aEpoxy matrix composites. 615 7$aFiber composites. 615 7$aFinite element method. 615 7$aHoneycomb structures. 615 7$aRobustness (mathematics) 615 7$aSandwich structures. 700 $aMyers$b David E$c(Engineer),$0328638 702 $aPineda$b Evan J. 712 02$aNASA Glenn Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 801 2$bGPO 801 2$bDIBIB 801 2$bLWA 801 2$bOCLCO 801 2$bOCLCF 801 2$bINT 801 2$bOCLCQ 801 2$bOCLCO 801 2$bXFF 801 2$bOCL 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910705251203321 996 $aBuckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel$93539258 997 $aUNINA