LEADER 02513oam 2200697I 450 001 9910707334103321 005 20160802131408.0 035 $a(CKB)5470000002464179 035 $a(OCoLC)846225982 035 $a(EXLCZ)995470000002464179 100 $a20130602j199612 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPrediction of composite laminate fracture: micromechanics and progressive fracture /$fP.K. Gotsis and C.C. Chamis, L. Minnetyan 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1996. 215 $a1 online resource (14 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v107331 300 $aTitle from title screen (viewed July 26, 2016). 300 $a"December 1996." 300 $a"Performing organization: National National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 7). 517 $aPrediction of composite laminate fracture 606 $aGlass fibers$2nasat 606 $aGraphite-epoxy composites$2nasat 606 $aMatrix materials$2nasat 606 $aLaminates$2nasat 606 $aEpoxy matrix composites$2nasat 606 $aResidual stress$2nasat 606 $aStress-strain relationships$2nasat 606 $aGraphite$2nasat 606 $aFiber composites$2nasat 606 $aComposite materials$2nasat 606 $aFracture mechanics$2nasat 615 7$aGlass fibers. 615 7$aGraphite-epoxy composites. 615 7$aMatrix materials. 615 7$aLaminates. 615 7$aEpoxy matrix composites. 615 7$aResidual stress. 615 7$aStress-strain relationships. 615 7$aGraphite. 615 7$aFiber composites. 615 7$aComposite materials. 615 7$aFracture mechanics. 700 $aGotsis$b Pascal K.$01403192 702 $aChamis$b C. C$g(Christos C.), 702 $aMinnetyan$b Levon$f1946- 712 02$aLewis Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910707334103321 996 $aPrediction of composite laminate fracture: micromechanics and progressive fracture$93487276 997 $aUNINA