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NACA-TN-1348

Critical shear stress of curved rectangular panels

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:37:50Z
date available2017-09-04T16:37:50Z
date copyright01/01/1947
date issued1947
identifier otherVGNSYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/101337
description abstractINTRODUCTION
A series of papers has been prepared to provide information on the buckling of curved sheet. The problem treated in the present paper, which is a part of that series, is the determination Of the critical shear stress of a cylindrical curved rectangular panel. For panels having simply supported edges this problem is solved theoretically (see appendix), and computed curves are provided for finding the critical shear stress. Estimated results are also given for curved rectangular panels having clamped edges.
languageEnglish
titleNACA-TN-1348num
titleCritical shear stress of curved rectangular panelsen
typestandard
page30
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsBENDING
subject keywordsBUCKLING
subject keywordsCURVED
subject keywordsDONNELL
subject keywordsFLAT
subject keywordsLOADS
subject keywordsPLATES
subject keywordsRECTANGULAR
subject keywordsSHEAR
subject keywordsSHEARING
subject keywordsSKIN
subject keywordsSTRESSED
subject keywordsSTRESSES
subject keywordsTHEORIES
subject keywordsTORSION


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