LEADER 01613nam  2200469Ia 450 
001 9910699801203321
005 20110624143508.0
035   $a(CKB)5470000002404929
035   $a(OCoLC)700073286
035   $a(EXLCZ)995470000002404929
100   $a20110202d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of a benchmark example for delamination fatigue growth prediction$b[electronic resource] /$fRonald Krueger
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (46 pages) $cillustrations
225 1 $aNASA/CR-2010-216723
300   $aTitle from title screen (viewed on Feb. 2, 2011).
300   $a"July 2010."
300   $a"NIA Report No. 2010-04."
320   $aIncludes bibliographical references (page 207).
606   $aDelaminating$2nasat
606   $aComposite materials$2nasat
606   $aFinite element method$2nasat
606   $aCyclic loads$2nasat
606   $aMathematical models$2nasat
615  7$aDelaminating.
615  7$aComposite materials.
615  7$aFinite element method.
615  7$aCyclic loads.
615  7$aMathematical models.
700   $aKrueger$b Ronald$01395935
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699801203321
996   $aDevelopment of a benchmark example for delamination fatigue growth prediction$93496602
997   $aUNINA