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: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1705.
Subjects:
ISBN: 9781680156140
1680156144
Physical Description: 1 online resource (17 pages) : illustrations

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