LEADER 01958nam  2200517Ia 450 
001 9910701854603321
005 20120625141808.0
035   $a(CKB)5470000002421562
035   $a(OCoLC)796619364
035   $a(EXLCZ)995470000002421562
100   $a20120625d2011      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates$b[electronic resource] /$fEvan J. Pineda, Anthony M. Waas
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (59 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2011-217401
300   $aTitle from title screen (viewed on June 25, 2012).
300   $a"December 2011."
320   $aIncludes bibliographical references (pages 55-59).
606   $aFiber composites$2nasat
606   $aPlastic deformation$2nasat
606   $aComputational grids$2nasat
606   $aDamage$2nasat
606   $aFiber orientation$2nasat
606   $aFinite element method$2nasat
606   $aLaminates$2nasat
615  7$aFiber composites.
615  7$aPlastic deformation.
615  7$aComputational grids.
615  7$aDamage.
615  7$aFiber orientation.
615  7$aFinite element method.
615  7$aLaminates.
700   $aPineda$b Evan J$01387412
701   $aWaas$b Anthony M$0961348
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701854603321
996   $aNumerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates$93437225
997   $aUNINA