01802nam 2200529 450 991070622020332120171030152709.0(CKB)5470000002456238(OCoLC)1008595885(EXLCZ)99547000000245623820171030j200004 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAdvances in fatigue and fracture mechanics analyses for metallic aircraft structures /J.C. Newman, JrHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,April 2000.1 online resource (40 pages) illustrationsNASA/TM ;2000-210084"April 2000.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 19-24).Aircraft structuresnasatCracksnasatFinite element methodnasatFracture mechanicsnasatStress analysisnasatMetalsnasatCrack propagationnasatMetal fatiguenasatAircraft structures.Cracks.Finite element method.Fracture mechanics.Stress analysis.Metals.Crack propagation.Metal fatigue.Newman J. C.878389Langley Research Center,GPOGPOBOOK9910706220203321Advances in fatigue and fracture mechanics analyses for metallic aircraft structures3454909UNINA