Experimental investigation of the effects of plastic flow in a tension panel with a circular hole
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1948 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
4,250 words, Guess
Page Count
17 pages
Identifiers
- ISBN-101680156144
- ISBN-139781680156140
- OCLC Control Number919094518
- Open LibraryOL44477750M
Classifications
- DDC620.186
- LCCTA480.A6
Description
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 stress concentration factor is appreciably reduced and the strain concentration factor is appreciably increased. Subjecting the panels to 100 repeated loading cycles caused no change to occur in the maximum values of the stress and strain concentration factors.
Subjects
Series Statement
- National Advisory Committee for Aeronautics technical note -- number 1705
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1705.
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