NACA-TN-1851
Critical shear stress of infinitely long, simply supported plate with transverse stiffeners
Year: 1949
Abstract: A theoretical solution is given for the critical shear stress of an infinitely long, simply supported, flat plate with identical, equally spaced, transverse stiffeners of zero tensional stiffness. Results are obtained by means of the Lagrangian multiplier method and are presented in the form of design charts. Experimental results are included and are found to be in good agreement with the theoretical results.
Subject: ALCOA
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contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T16:56:17Z | |
date available | 2017-09-04T16:56:17Z | |
date copyright | 01/01/1949 | |
date issued | 1949 | |
identifier other | XDPTYDAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/119773 | |
description abstract | A theoretical solution is given for the critical shear stress of an infinitely long, simply supported, flat plate with identical, equally spaced, transverse stiffeners of zero tensional stiffness. Results are obtained by means of the Lagrangian multiplier method and are presented in the form of design charts. Experimental results are included and are found to be in good agreement with the theoretical results. | |
language | English | |
title | NACA-TN-1851 | num |
title | Critical shear stress of infinitely long, simply supported plate with transverse stiffeners | en |
type | standard | |
page | 40 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1949 | |
contenttype | fulltext | |
subject keywords | ALCOA | |
subject keywords | ALLOYS | |
subject keywords | ALUMINUM | |
subject keywords | BEAMS | |
subject keywords | BUCKLING | |
subject keywords | CHARTS | |
subject keywords | FLAT | |
subject keywords | PLATES | |
subject keywords | SHEAR | |
subject keywords | SKIN | |
subject keywords | STRENGTH | |
subject keywords | STRESSED | |
subject keywords | WEBS |