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NACA-WRL-258

EFFECT OF NORMAL PRESSURE ON THE CRITICAL COMPRESSIVE STRESS OF CURVED SHEET

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:48:00Z
date available2017-09-04T16:48:00Z
date copyright08/25/1942
date issued1942
identifier otherWGYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/111429
description abstractResults are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. (author)
languageEnglish
titleNACA-WRL-258num
titleEFFECT OF NORMAL PRESSURE ON THE CRITICAL COMPRESSIVE STRESS OF CURVED SHEETen
typestandard
page9
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsATMOSPHERIC PRESSURE
subject keywordsBUCKLING
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsCRITICAL LOADING
subject keywordsCURVED PANELS
subject keywordsLOAD TESTS
subject keywordsPRESSURE EFFECTS
subject keywordsREINFORCEMENT (STRUCTURES)
subject keywordsRIBS (SUPPORTS)
subject keywordsSHEETS
subject keywordsSPACING


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