01792nam 2200493 450 991070791190332120170223102232.0(CKB)5470000002469454(OCoLC)973486608(EXLCZ)99547000000246945420170223j199611 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAnalytical methodology for predicting the onset of widespread fatigue damage in fuselage structure /C.E. Harris [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,November 1996.1 online resource (25 pages) illustrationsNASA technical memorandum ;110293"November 1996.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 15-16).FuselagesnasatResidual strengthnasatCrack initiationnasatCrack propagationnasatFatigue (materials)nasatComputer programsnasatFuselages.Residual strength.Crack initiation.Crack propagation.Fatigue (materials)Computer programs.Harris Charles E.1950-1395080Abeyounis William KellyLangley Research Center,GPOGPOBOOK9910707911903321Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure3467457UNINA