LEADER 01908nam  2200505Ia 450 
001 9910699315103321
005 20230902161818.0
035   $a(CKB)5470000002402769
035   $a(OCoLC)724603603
035   $a(EXLCZ)995470000002402769
100   $a20110517d2006      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInfluence of finite element software on energy release rates computed using the virtual crack closure technique$b[electronic resource] /$fRonald Krueger, Dirk Goetze
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2006]
215   $a1 online resource (49 pages) $cillustrations (some color)
225 1 $aNAS/CR ;$v2006-214523
300   $aTitle from title screen (viewed on May 16, 2011).
300   $a"October 2006."
300   $a"Prepared for Langley Research Center."
300   $a"National Institute of Aerospace."
300   $a"NIA Report no. 2006-06."
320   $aIncludes bibliographical references (pages 15-17).
410  0$aNASA contractor report ;$vNAS/CR-2006-214523.
606   $aFinite element method$2nasat
606   $aStrain energy release rate$2nasat
606   $aCrack closure$2nasat
606   $aDelaminating$2nasat
615  7$aFinite element method.
615  7$aStrain energy release rate.
615  7$aCrack closure.
615  7$aDelaminating.
700   $aKrueger$b Ronald$01395935
701   $aGoetze$b Dirk$01395936
712 02$aLangley Research Center.
712 02$aNational Institute of Aerospace.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699315103321
996   $aInfluence of finite element software on energy release rates computed using the virtual crack closure technique$93455213
997   $aUNINA