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contributor authorArchibald N. Sherbourne
contributor authorOsama K. Bedair
date accessioned2017-05-08T22:36:50Z
date available2017-05-08T22:36:50Z
date copyrightOctober 1993
date issued1993
identifier other%28asce%290733-9399%281993%29119%3A10%281956%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/83797
description abstractThe postbuckling behavior of plate‐stiffener assemblies in uniform axial compression is investigated in which the energy method is used to model various in and out‐of‐plane boundary conditions. The loaded edges are treated as simply supported and remain straight. The unloaded edges can be simply supported or elastically restrained against rotation. Beside these out‐of‐plane boundary conditions, the in‐plane boundary condition for the unloaded edges may be any of the following: free translation, fully restrained against translation, straight, free to bend, and partially restrained against in‐plane bending. Analytical expressions for the membrane strain energy for each of these boundary conditions for any plate aspect ratio are derived and the geometric properties of the stiffeners that dictate these boundary conditions are defined in the paper. Typical numerical results are obtained for square plates and the influence of these boundary conditions on the load‐deflection and load‐end shortening behavior is illustrated.
publisherAmerican Society of Civil Engineers
titlePlate‐Stiffener Assemblies in Uniform Compression. Part II: Postbuckling
typeJournal Paper
journal volume119
journal issue10
journal titleJournal of Engineering Mechanics
identifier doi10.1061/(ASCE)0733-9399(1993)119:10(1956)
treeJournal of Engineering Mechanics:;1993:;Volume ( 119 ):;issue: 010
contenttypeFulltext


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