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contributor authorNicholas J. Hoff
date accessioned2017-05-08T23:29:15Z
date available2017-05-08T23:29:15Z
date copyrightMarch, 1965
date issued1965
identifier issn0021-8936
identifier otherJAMCAV-25796#71_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105001
description abstractAnalysis of the simple model proposed yields equilibrium curves in agreement with those obtained by other investigators for axially compressed, thin-walled, circular cylindrical shells. A rigorous calculation of the stability of the equilibrium of the model indicates that the snap-through phenomenon can be entirely absent when an imperfect shell is heated in a perfectly rigid testing machine. When the testing machine is sufficiently elastic, snap through will occur. It may take place at a temperature smaller than, equal-to, or greater than T = εcr /α, where εcr is the theoretical critical strain of the perfect shell and α is the coefficient of expansion of the material of the shell, but the maximum stress produced in the imperfect shell will always be less than εcr E, where E is Young’s modulus of the material.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Nonlinear Model Study of the Thermal Buckling of Thin Elastic Shells
typeJournal Paper
journal volume32
journal issue1
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3625786
journal fristpage71
journal lastpage75
identifier eissn1528-9036
keywordsBuckling
keywordsShells
keywordsEquilibrium (Physics)
keywordsTesting
keywordsMachinery
keywordsStress
keywordsStability
keywordsElasticity
keywordsTemperature AND Circular cylindrical shells
treeJournal of Applied Mechanics:;1965:;volume( 032 ):;issue: 001
contenttypeFulltext


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