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001 9910703588603321
005 20150227142658.0
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035   $a(OCoLC)904156949
035   $a(EXLCZ)995470000002431811
100   $a20150227j201402    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBi-metallic composite structures with designed internal residual stress field /$fCraig A. Brice
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2014.
215   $a1 online resource (10 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218174
300   $aTitle from title screen (viewed Feb. 27, 2015).
300   $a"February 2014."
320   $aIncludes bibliographical references (page 4).
606   $aBimetals$2nasat
606   $aResidual stress$2nasat
606   $aShape memory alloys$2nasat
606   $aPhase transformations$2nasat
606   $aPowder metallurgy$2nasat
606   $aCrack propagation$2nasat
615  7$aBimetals.
615  7$aResidual stress.
615  7$aShape memory alloys.
615  7$aPhase transformations.
615  7$aPowder metallurgy.
615  7$aCrack propagation.
700   $aBrice$b Craig A.$01394162
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703588603321
996   $aBi-metallic composite structures with designed internal residual stress field$93546601
997   $aUNINA