01795nam 2200529I 450 991070790510332120170322081657.0(CKB)5470000002469522(OCoLC)973932631(EXLCZ)99547000000246952220170228j199701 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFatigue-life prediction methodology using small-crack theory /J.C. Newman, Jr. and E.P. Phillips, M.H. SwainHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,January 1997.1 online resource (29 pages) illustrationsNASA technical memorandum ;110307"January 1997.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 26-29).Crack closurenasatFatigue lifenasatCrack propagationnasatPlastic propertiesnasatStress intensity factorsnasatModelsnasatCrack tipsnasatCrack closure.Fatigue life.Crack propagation.Plastic properties.Stress intensity factors.Models.Crack tips.Newman J. C.878389Phillips Edward P.Swain M. H.Langley Research Center,GPOGPOBOOK9910707905103321Fatigue-life prediction methodology using small-crack theory3463085UNINA