01655oam 2200445I 450 991070686110332120180227144422.0(CKB)5470000002458856(OCoLC)1024083482(OCoLC)995470000002458856(EXLCZ)99547000000245885620180223j194701 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension /by L. Ross Levin and David H. NelsonWashington :National Advisory Committee for Aeronautics,January 1947.1 online resource (10 pages, 6 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 1177"January 1947."Distribution made by issuing office.Includes bibliographical references (page 9).RivetsnasatAluminum alloysnasatAeronauticsnasatRivets.Aluminum alloys.Aeronautics.Levin L. Ross1420497Nelson David H.United States.National Advisory Committee for Aeronautics,GPOGPOGPOBOOK9910706861103321Effect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension3538476UNINA