LEADER 02244oam  2200553Ia 450 
001 9910702121403321
005 20121031075307.0
035   $a(CKB)5470000002424927
035   $a(OCoLC)742768423
035   $a(EXLCZ)995470000002424927
100   $a20120810d2010      ua             0
101 0 $aund
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aComputational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates$b[electronic resource] /$fEvan J. Pineda ... [and others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (22 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217243
300   $aTitle from title screen (viewed on Oct. 29, 2012).
300   $a"Prepared for the 51th Structures, Structural Dynamics, and Materials Conference cosponsored by the AIAA, ASME, ASCE, AHS, and ASC Orlando, Florida, April 12-15, 2010."
300   $a"May 2012."
300   $a"AIAA-2010-2815."
320   $aIncludes bibliographical references (pages 21-22).
606   $aFiber composites$2nasat
606   $aLaminates$2nasat
606   $aContinuums$2nasat
606   $aFailure analysis$2nasat
606   $aMicrocracks$2nasat
606   $aPotential theory$2nasat
606   $aTransverse loads$2nasat
615  7$aFiber composites.
615  7$aLaminates.
615  7$aContinuums.
615  7$aFailure analysis.
615  7$aMicrocracks.
615  7$aPotential theory.
615  7$aTransverse loads.
701   $aPineda$b Evan J$01387412
712 02$aNASA Glenn Research Center.
712 12$aAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference$d(51st :$f2012 :$eOrlando, Fla.)
801  0$bEYM
801  1$bEYM
801  2$bGPO
906   $aBOOK
912   $a9910702121403321
996   $aComputational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates$93530620
997   $aUNINA