02085oam 2200565 450 991071376680332120210128063552.0(CKB)5470000002504014(OCoLC)1099802663(EXLCZ)99547000000250401420190503d1947 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe 1350°F stress-rupture properties of two wrought alloys and three cast alloys /by E.E. Reynolds, J.W. Freeman, and A.E. WhiteWashington, [D.C.] :National Advisory Committee for Aeronautics,1947.1 online resource (23 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 1380"November 1947."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 7).One thousand three hundred fifty degree fahrenheit stress-rupture properties of two wrought alloys and three cast alloysAlloysEffect of temperature onAlloysFatigueTestingStrains and stressesAlloysFatigueTestingfastStrains and stressesfastAlloysEffect of temperature on.AlloysFatigueTesting.Strains and stresses.AlloysFatigueTesting.Strains and stresses.Reynolds E. E.193386Freeman J. W(James W.),White A. E(Albert Easton),1884-1956,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOSTFGPOBOOK9910713766803321The 1350°F stress-rupture properties of two wrought alloys and three cast alloys3503330UNINA