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contributor authorVictor Birman
date accessioned2017-05-08T23:31:39Z
date available2017-05-08T23:31:39Z
date copyrightDecember, 1990
date issued1990
identifier issn0021-8936
identifier otherJAMCAV-26328#941_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106353
description abstractThermal dynamic problems of circular cylindrical composite shells reinforced in the axial and circumferential directions and subject to variations of temperature are considered. Nonlinear governing equations are formulated based on the extension of Donnell shell theory. These equations are used to determine the response of geometrically nonlinear and linear shells to a thermal loading represented by the Heaviside step function (thermal shock). The solution of the nonlinear problem obtained by the assumption that displacements are single-term functions of coordinates is discussed. The analysis of the linear problem illustrates different types of response to thermal shock. The condition of thermally-induced buckling of shells is formulated. Numerical analysis results in conclusions regarding the behavior of shells subject to thermal shock if the temperature is uniformly distributed throughout the shell and stiffeners.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Dynamic Problems of Reinforced Composite Cylinders
typeJournal Paper
journal volume57
journal issue4
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.2897665
journal fristpage941
journal lastpage947
identifier eissn1528-9036
keywordsComposite materials
keywordsCylinders
keywordsShells
keywordsThermal shock
keywordsTemperature
keywordsEquations
keywordsFunctions
keywordsNumerical analysis AND Buckling
treeJournal of Applied Mechanics:;1990:;volume( 057 ):;issue: 004
contenttypeFulltext


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