02172oam 2200589 450 991071606130332120210512093505.0(CKB)5470000002517491(OCoLC)785108102(OCoLC)50500050(OCoLC)760937021(EXLCZ)99547000000251749120120408j196901 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierTensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) /by Dick M. RoysterWashington, D.C. :National Aeronautics and Space Administration,January 1969.1 online resource (42 pages) illustrationsNASA/TN ;D-5010"January 1969."Includes bibliographical references (page 12).Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F Tensile propertiesnasatAluminum alloysDuctilityAluminum alloysCreepSupersonic transport planesMaterialsEnvironmental testingAluminum alloysCreepfastAluminum alloysDuctilityfastTensile properties.Aluminum alloysDuctility.Aluminum alloysCreep.Supersonic transport planesMaterialsEnvironmental testing.Aluminum alloysCreep.Aluminum alloysDuctility.Royster Dick M.1399411United States.National Aeronautics and Space Administration,OCLCEOCLCEABCAD#OCLCQOCLCOOCLCQOCLCFOCLCQCOPGPOBOOK9910716061303321Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K)3486920UNINA