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NACA-ARR-4B03

Compressive strength of flat panels with Z-section stiffeners

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:42:10Z
date available2017-09-04T16:42:10Z
date copyright01/01/1944
date issued1944
identifier otherVRCTUDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/105499
description abstractINTRODUCTION
Several series of compression tests have been made on panels with Z-section stiffeners formed from flat sheet (see fig.1) to show the importance of relative dimensions in determining the strength of the panels. The average compressive stresses at maximum load and the buckling stresses for the sheet obtained in the investigation are presented in this report, which is an extension of reference 1 and which supersedes this reference.
languageEnglish
titleNACA-ARR-4B03num
titleCompressive strength of flat panels with Z-section stiffenersen
typestandard
page20
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1944
contenttypefulltext
subject keywordsALCOA
subject keywordsALLOY
subject keywordsALLOYS
subject keywordsALUMINUM
subject keywordsCOMBINATIONS
subject keywordsCOMPRESSIVE
subject keywordsCOUNTRSUNK
subject keywordsRIVETS
subject keywordsSHEET
subject keywordsSHEETS
subject keywordsSKIN
subject keywordsSTIFFENER
subject keywordsSTRENGTH
subject keywordsSTRESSED


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