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Buckling stresses of simply supported rectangular flat plates in shea

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:26:35Z
date available2017-09-04T18:26:35Z
date copyright01/01/1947
date issued1947
identifier otherILYIYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/208819
description abstractINTRODUCTION
In reference 1 Timoshenko presents a solution for the buckling stresses of simply supported rectangular flat plates in shear. Timoshenko considered only the equations which permitted a buckle pattern symmetric about the midpoint of the plate. This limitation led to a small error in the critical stress in several cases in which the governing buckle pattern was antisymmetric instead of symmetric.
The buckling stresses have been determined more correctly than in reference 1 by considering both the symmetric and the antisymmetric buckle patterns. Through the use of the matrix iteration method described in reference 2 and by a proper choice of the terms in the series representing the deflection, more accurate results were obtained. The theoretical analysis given in the appendix is a brief summary of the derivation given in reference 1.
languageEnglish
titleNACA-TN-1222num
titleBuckling stresses of simply supported rectangular flat plates in sheaen
typestandard
page14
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsBUCKLING
subject keywordsFLAT
subject keywordsFORMULAS
subject keywordsLOADS
subject keywordsPLATES
subject keywordsRECTANGULAR
subject keywordsSHEAR
subject keywordsSTRESSES


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