01735oam 2200493 450 991071523140332120210323105123.0(CKB)5470000002509712(OCoLC)1233179499(OCoLC)995470000002509712(EXLCZ)99547000000250971220210128j202004 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEvaluation of fatigue damage accumulation functions for delamination initiation and propagation /Carlos G. Dávila [and four others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,April 2020.1 online resource (ii, 32 pages, 1 unnumbered page) color illustrationsNASA/TP ;2020-220584"April 2020."Includes bibliographical references (pages 31-32).Composite materialsDelaminationComposite materialsDelaminationfastCrack propagationnasatFatigue lifenasatCyclic loadsnasatComposite materialsDelamination.Composite materialsDelamination.Crack propagation.Fatigue life.Cyclic loads.Davila Carlos G.1412406Langley Research Center,GPOGPOOCLCOOCLCFGPOBOOK9910715231403321Evaluation of fatigue damage accumulation functions for delamination initiation and propagation3522076UNINA