Stress-strain and elongation graphs for Alclad aluminum-alloy 24S-T86 sheet / James A. Miller.

Results of tests on duplicate longitudinal and transverse specimens of Alclad aluminum-alloy 24S-T86 sheets with norminal thicknesses of 0.032, 0.064, and 0.125 inch are presented in the form of graphs. Tensile and compressive stress-strain graphs and stress-deviation graphs to a strain of about 1 p...

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Bibliographic Details
Main Author: Miller, James A.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2094.
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Call Number: Y 3.N 21/5:6/2094
Y 3.N 21/5:6/2094 Available Place a Hold