01889nam 2200553 450 991070619100332120170817142744.0(CKB)5470000002454513(OCoLC)1001296703(EXLCZ)99547000000245451320170817j199812 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMethodology for predicting the onset of widespread fatigue damage in lap-splice joints /J.C. Newman, Jr. [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1998.1 online resource (15 pages) illustrationsNASA/TM ;1998-208975"December 1998.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 10-11).Crack propagationnasatCrack tipsnasatAirframesnasatStress analysisnasatLap jointsnasatFuselagesnasatFinite element methodnasatFatigue testsnasatFatigue (materials)nasatCrack propagation.Crack tips.Airframes.Stress analysis.Lap joints.Fuselages.Finite element method.Fatigue tests.Fatigue (materials)Newman J. C.878389Langley Research Center,GPOGPOBOOK9910706191003321Methodology for predicting the onset of widespread fatigue damage in lap-splice joints3497635UNINA