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001 9910706191003321
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035   $a(EXLCZ)995470000002454513
100   $a20170817j199812    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMethodology for predicting the onset of widespread fatigue damage in lap-splice joints /$fJ.C. Newman, Jr. [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1998.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208975
300   $a"December 1998."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 10-11).
606   $aCrack propagation$2nasat
606   $aCrack tips$2nasat
606   $aAirframes$2nasat
606   $aStress analysis$2nasat
606   $aLap joints$2nasat
606   $aFuselages$2nasat
606   $aFinite element method$2nasat
606   $aFatigue tests$2nasat
606   $aFatigue (materials)$2nasat
615  7$aCrack propagation.
615  7$aCrack tips.
615  7$aAirframes.
615  7$aStress analysis.
615  7$aLap joints.
615  7$aFuselages.
615  7$aFinite element method.
615  7$aFatigue tests.
615  7$aFatigue (materials)
700   $aNewman$b J. C.$0878389
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706191003321
996   $aMethodology for predicting the onset of widespread fatigue damage in lap-splice joints$93497635
997   $aUNINA