LEADER 01792nam  2200493   450 
001 9910707911903321
005 20170223102232.0
035   $a(CKB)5470000002469454
035   $a(OCoLC)973486608
035   $a(EXLCZ)995470000002469454
100   $a20170223j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalytical methodology for predicting the onset of widespread fatigue damage in fuselage structure /$fC.E. Harris [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1996.
215   $a1 online resource (25 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110293
300   $a"November 1996."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 15-16).
606   $aFuselages$2nasat
606   $aResidual strength$2nasat
606   $aCrack initiation$2nasat
606   $aCrack propagation$2nasat
606   $aFatigue (materials)$2nasat
606   $aComputer programs$2nasat
615  7$aFuselages.
615  7$aResidual strength.
615  7$aCrack initiation.
615  7$aCrack propagation.
615  7$aFatigue (materials)
615  7$aComputer programs.
700   $aHarris$b Charles E.$f1950-$01395080
702   $aAbeyounis$b William Kelly
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707911903321
996   $aAnalytical methodology for predicting the onset of widespread fatigue damage in fuselage structure$93467457
997   $aUNINA