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NASA-TN-D-360

Bending and compression tests of pressurized ring-stiffened cylinders

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:18:30Z
date available2017-09-04T18:18:30Z
date copyright01/01/1960
date issued1960
identifier otherHRTKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/201265
description abstractThe results of tests on pressurized ring-stiffened cylinders subjected to compression and bending are presented and discussed. The results obtained at high values of internal pressure differ from those obtained by previous investigators in that the theoretical small-deflection compressive buckling coefficient of 0.6 was nearly achieved in each test. Small amounts of internal pressure had a greater stabilizing effect in the bending tests than in the compression tests.
languageEnglish
titleNASA-TN-D-360num
titleBending and compression tests of pressurized ring-stiffened cylindersen
typestandard
page28
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsBEND
subject keywordsBUCKLING
subject keywordsCOMPRESSION
subject keywordsCYLINDRICAL
subject keywordsDEFLECTION
subject keywordsDEPENDENCE
subject keywordsINTERNAL
subject keywordsLOADS
subject keywordsPRESSURE
subject keywordsPRESSURIZING
subject keywordsREINFORCEMENT
subject keywordsRINGS
subject keywordsSHELLS
subject keywordsSTABILITY
subject keywordsSTRUCTURAL
subject keywordsTESTS
subject keywordsTHICKNESS


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