LEADER 01935nam  2200529Ia 450 
001 9910701781203321
005 20120531135115.0
035   $a(CKB)5470000002420283
035   $a(OCoLC)794557657
035   $a(EXLCZ)995470000002420283
100   $a20120531d2011      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 mode II static delamination propagation and fatigue growth predictions$b[electronic resource] /$fRonald Krueger
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center :$cNational Institute of Aerospace,$d[2011]
215   $a1 online resource (68 pages) $ccolor illustrations
225 1 $a[NASA contractor report] ;$vNASA/CR-2011-217305
300   $aTitle from title screen (viewed on May 31, 2012).
300   $a"November 2011."
300   $a"NIA report no. 2011-02."
320   $aIncludes bibliographical references.
606   $aDelaminating$2nasat
606   $aMathematical models$2nasat
606   $aFatigue (materials)$2nasat
606   $aFlexing$2nasat
606   $aCrack closure$2nasat
606   $aStress propagation$2nasat
606   $aStatic loads$2nasat
615  7$aDelaminating.
615  7$aMathematical models.
615  7$aFatigue (materials)
615  7$aFlexing.
615  7$aCrack closure.
615  7$aStress propagation.
615  7$aStatic loads.
700   $aKrueger$b Ronald$01395935
712 02$aLangley Research Center.
712 02$aNational Institute of Aerospace.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701781203321
996   $aDevelopment and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions$93467746
997   $aUNINA