Combined-stress fatigue strength of 76S-T61 aluminum alloy with superimposed mean stresses and corrections for yielding /

Fatigue data for 76S-T61aluminum alloy are presented for several combinations of bending and torsion with both alternating and mean stresses. Special fatigue equipment for these tests is described. Correction ofr yielding was applied to the mean stresses in the bending and in the torsion fatigue tes...

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Bibliographic Details
Main Author: Findley, William N (William Nichols)
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1953
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2924
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Stanford University

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Call Number: NACA TN 2924