LEADER 02027nam  2200553Ia 450 
001 9910702212103321
005 20121109094104.0
035   $a(CKB)5470000002426031
035   $a(OCoLC)816637837
035   $a(EXLCZ)995470000002426031
100   $a20121109d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of benchmark examples to assess the single and mixed-mode static delamination propagation capabilities in ANSYSŪ$b[electronic resource] /$fRonald Krueger
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center :$cNational Institute of Aerospace,$d[2012]
215   $a1 online resource (66 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2012-217588
300   $aTitle from title screen (viewed on Nov. 9, 2012).
300   $a"July 2012."
300   $a"NIA Report No. 2012-04."
320   $aIncludes bibliographical references (page 22).
606   $aDelaminating$2nasat
606   $aStatic loads$2nasat
606   $aFracture mechanics$2nasat
606   $aCrack propagation$2nasat
606   $aFinite element method$2nasat
606   $aAutomatic control$2nasat
606   $aTwo dimensional$2nasat
606   $aMechanical properties$2nasat
615  7$aDelaminating.
615  7$aStatic loads.
615  7$aFracture mechanics.
615  7$aCrack propagation.
615  7$aFinite element method.
615  7$aAutomatic control.
615  7$aTwo dimensional.
615  7$aMechanical properties.
700   $aKreuger$b Ronald$01411717
712 02$aLangley Research Center.
712 02$aNational Institute of Aerospace.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702212103321
996   $aApplication of benchmark examples to assess the single and mixed-mode static delamination propagation capabilities in ANSYSŪ$93503588
997   $aUNINA