Experimental investigation of the effects of plastic flow in a tension panel with a circular hole /

Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the...

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Bibliographic Details
Main Author: Griffith, George E. (Author)
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1705
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