LEADER 01755nam  2200469I  450 
001 9910703786503321
005 20150826160626.0
035   $a(CKB)5470000002433853
035   $a(OCoLC)919219070
035   $a(EXLCZ)995470000002433853
100   $a20150826j201502    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCharacterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy /$fJohn A. New [and seven others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2015.
215   $a1 online resource (20 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218685
300   $aTitle from title screen (viewed Aug. 26, 2015).
300   $a"February 2015."
320   $aIncludes bibliographical references (pages 18-20).
606   $aSpacecraft structures$2nasat
606   $aAluminum alloys$2nasat
606   $aFriction stir welding$2nasat
606   $aResidual stress$2nasat
606   $aStress intensity factors$2nasat
615  7$aSpacecraft structures.
615  7$aAluminum alloys.
615  7$aFriction stir welding.
615  7$aResidual stress.
615  7$aStress intensity factors.
700   $aNew$b John A.$01416405
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703786503321
996   $aCharacterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy$93521641
997   $aUNINA