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035   $a(OCoLC)945556941
035   $a(EXLCZ)995470000002461049
100   $a20160324j199710    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses /$fEdward P. Phillips
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1997.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4784
300   $aTitle from title screen (viewed March 24, 2016).
300   $a"October 1997."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aCrack propagation$2nasat
606   $aFatigue (materials)$2nasat
606   $aAluminum$2nasat
606   $aBending fatigue$2nasat
606   $aAluminum alloys$2nasat
615  7$aCrack propagation.
615  7$aFatigue (materials)
615  7$aAluminum.
615  7$aBending fatigue.
615  7$aAluminum alloys.
700   $aPhillips$b Edward P.$01412274
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707044003321
996   $aAn experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses$93505284
997   $aUNINA