LEADER 01737nam  2200517Ia 450 
001 9910697164503321
005 20230902161857.0
035   $a(CKB)5470000002385266
035   $a(OCoLC)696008010
035   $a(EXLCZ)995470000002385266
100   $a20110110d2006      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 02$aA thermodynamically consistent damage model for advanced composites$b[electronic resource] /$fPere Maimi? ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2006]
215   $a1 online resource (42 pages) $cillustrations
225 1 $aNASA/TM- ;$v2006-214282
300   $aTitle from title screen (viewed on Jan. 10, 2011).
300   $a"March 2006."
320   $aIncludes bibliographical references (pages 34-37).
410  0$aNASA technical memorandum ;$v214282.
606   $aComposite materials$2nasat
606   $aDamage$2nasat
606   $aContinuum modeling$2nasat
606   $aFiber composites$2nasat
606   $aCrack closure$2nasat
606   $aDegradation$2nasat
606   $aLoads (forces)$2nasat
615  7$aComposite materials.
615  7$aDamage.
615  7$aContinuum modeling.
615  7$aFiber composites.
615  7$aCrack closure.
615  7$aDegradation.
615  7$aLoads (forces)
701   $aMaimi?$b Pere$01415407
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697164503321
996   $aA thermodynamically consistent damage model for advanced composites$93517339
997   $aUNINA