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NACA-TN-2021

Buckling of Thin-Walled Cylinder under Axial Compression and Internal Pressure

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:49:26Z
date available2017-09-04T15:49:26Z
date copyright01/01/1950
date issued1950
identifier otherQDYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/52402
description abstractAn investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results. (author)
languageEnglish
titleNACA-TN-2021num
titleBuckling of Thin-Walled Cylinder under Axial Compression and Internal Pressureen
typestandard
page30
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1950
contenttypefulltext
subject keywordsALUMINUM ALLOYS
subject keywordsANALOGIES
subject keywordsAXIAL COMPRESSION LOADS
subject keywordsBUCKLING
subject keywordsCOMPUTATION
subject keywordsCYLINDERS
subject keywordsCYLINDRICAL SHELLS
subject keywordsDEFLECTION
subject keywordsEXPERIMENTATION
subject keywordsINTERNAL PRESSURE
subject keywordsTHIN WALLED SHELLS


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