01847oam 2200517 450 991071729840332120220225123329.0(CKB)5470000002529237(OCoLC)1158388770(EXLCZ)99547000000252923720200615d1941 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of alternately high and low repeated stresses upon the fatigue strength of 25ST aluminum alloy /by G.W. StickleyWashington, [D.C.] :National Advisory Committee for Aeronautics,1941.1 online resource (5 pages, 1 unnumbered page) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 792"January 1941."No Federal Depository Library Program (FDLP) item number.Includes bibliographical reference (page 4).Aluminum alloysAlloysFatigueTestingStrains and stressesAlloysFatigueTestingfastAluminum alloysfastStrains and stressesfastAluminum alloys.AlloysFatigueTesting.Strains and stresses.AlloysFatigueTesting.Aluminum alloys.Strains and stresses.Stickley G. W.1420364United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717298403321Effect of alternately high and low repeated stresses upon the fatigue strength of 25ST aluminum alloy3537977UNINA