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001 9910707905103321
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035   $a(CKB)5470000002469522
035   $a(OCoLC)973932631
035   $a(EXLCZ)995470000002469522
100   $a20170228j199701    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue-life prediction methodology using small-crack theory /$fJ.C. Newman, Jr. and E.P. Phillips, M.H. Swain
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 1997.
215   $a1 online resource (29 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110307
300   $a"January 1997."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 26-29).
606   $aCrack closure$2nasat
606   $aFatigue life$2nasat
606   $aCrack propagation$2nasat
606   $aPlastic properties$2nasat
606   $aStress intensity factors$2nasat
606   $aModels$2nasat
606   $aCrack tips$2nasat
615  7$aCrack closure.
615  7$aFatigue life.
615  7$aCrack propagation.
615  7$aPlastic properties.
615  7$aStress intensity factors.
615  7$aModels.
615  7$aCrack tips.
700   $aNewman$b J. C.$0878389
702   $aPhillips$b Edward P.
702   $aSwain$b M. H.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707905103321
996   $aFatigue-life prediction methodology using small-crack theory$93463085
997   $aUNINA