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NACA-TN-1851

Critical shear stress of infinitely long, simply supported plate with transverse stiffeners

Organization:
NASA - National Aeronautics and Space Administration (NASA)
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.
URI: https://yse.yabesh.ir/std/handle/yse/119773
Subject: ALCOA
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NACA-TN-1851

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:56:17Z
date available2017-09-04T16:56:17Z
date copyright01/01/1949
date issued1949
identifier otherXDPTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/119773
description abstractA 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.
languageEnglish
titleNACA-TN-1851num
titleCritical shear stress of infinitely long, simply supported plate with transverse stiffenersen
typestandard
page40
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1949
contenttypefulltext
subject keywordsALCOA
subject keywordsALLOYS
subject keywordsALUMINUM
subject keywordsBEAMS
subject keywordsBUCKLING
subject keywordsCHARTS
subject keywordsFLAT
subject keywordsPLATES
subject keywordsSHEAR
subject keywordsSKIN
subject keywordsSTRENGTH
subject keywordsSTRESSED
subject keywordsWEBS
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