LEADER 01709nam  2200481I  450 
001 9910702005103321
005 20150825153743.0
035   $a(CKB)5470000002424082
035   $a(OCoLC)919174512
035   $a(EXLCZ)995470000002424082
100   $a20150825j201204    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment and application of benchmark examples for mixed-mode I/II quasi-static delamination propagation predictions /$fRonald Krueger
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2012.
215   $a1 online resource (57 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2012-217562
300   $aTitle from title screen (viewed Aug. 25, 2015).
300   $a"April 2012."
320   $aIncludes bibliographical references (page 18).
606   $aDelaminating$2nasat
606   $aFinite element method$2nasat
606   $aLoads (forces)$2nasat
606   $aCrack closure$2nasat
606   $aCantilever beams$2nasat
615  7$aDelaminating.
615  7$aFinite element method.
615  7$aLoads (forces)
615  7$aCrack closure.
615  7$aCantilever beams.
700   $aKrueger$b Ronald$01395935
712 02$aNational Institute of Aerospace.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702005103321
996   $aDevelopment and application of benchmark examples for mixed-mode I$93472343
997   $aUNINA