02095oam 2200601I 450 991071388660332120200824104113.0(CKB)5470000002504824(OCoLC)1100474456(EXLCZ)99547000000250482420190508d1954 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAdditional static and fatigue tests of high-strength aluminum-alloy bolted joints /by E.C. Hartmann, Marshall Holt, and I.D. EatonWashington, [D.C.] :National Advisory Committee for Aeronautics,1954.1 online resource (42 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3269"July 1954."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 14).Aluminum alloysFatigueBolted jointsTestingJoints (Engineering)Strength of materialsAluminum alloysFatiguefastBolted jointsTestingfastJoints (Engineering)fastStrength of materialsfastAluminum alloysFatigue.Bolted jointsTesting.Joints (Engineering)Strength of materials.Aluminum alloysFatigue.Bolted jointsTesting.Joints (Engineering)Strength of materials.Hartmann E. C.1415621Holt M(Marshall),Eaton I. D.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713886603321Additional static and fatigue tests of high-strength aluminum-alloy bolted joints3527532UNINA