01755nam 2200469I 450 991070378650332120150826160626.0(CKB)5470000002433853(OCoLC)919219070(EXLCZ)99547000000243385320150826j201502 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierCharacterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy /John A. New [and seven others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,February 2015.1 online resource (20 pages) color illustrationsNASA/TM ;2015-218685Title from title screen (viewed Aug. 26, 2015)."February 2015."Includes bibliographical references (pages 18-20).Spacecraft structuresnasatAluminum alloysnasatFriction stir weldingnasatResidual stressnasatStress intensity factorsnasatSpacecraft structures.Aluminum alloys.Friction stir welding.Residual stress.Stress intensity factors.New John A.1416405Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910703786503321Characterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy3521641UNINA