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contributor authorNicholas J. Hoff
contributor authorChi-Chang Chao
contributor authorWayne A. Madsen
date accessioned2017-05-08T23:17:58Z
date available2017-05-08T23:17:58Z
date copyrightJune, 1964
date issued1964
identifier issn0021-8936
identifier otherJAMCAV-25749#253_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98490
description abstractThe elastic stability of a thin-walled circular cylindrical shell is investigated by means of the small-deflection theory when the shell is subjected to such nonuniform heating as causes a uniform axial compressive stress to arise in a band of width 2b while the rest of the shell is free of stress. The critical value of the compressive axial stress is found to be equal to the critical stress of the same circular cylindrical shell when subjected to uniform axial compression provided the band is not extremely narrow. In the latter case the critical stress of the band is higher than that of the uniformly compressed shell.
publisherThe American Society of Mechanical Engineers (ASME)
titleBuckling of a Thin-Walled Circular Cylindrical Shell Heated Along an Axial Strip
typeJournal Paper
journal volume31
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3629594
journal fristpage253
journal lastpage258
identifier eissn1528-9036
keywordsBuckling
keywordsCircular cylindrical shells
keywordsStrips
keywordsStress
keywordsShells
keywordsStability
keywordsHeating
keywordsCompression
keywordsCompressive stress AND Deflection
treeJournal of Applied Mechanics:;1964:;volume( 031 ):;issue: 002
contenttypeFulltext


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