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contributor authorHabibollah Akbar
contributor authorAjaya K. Gupta
date accessioned2017-05-08T20:51:58Z
date available2017-05-08T20:51:58Z
date copyrightApril 1986
date issued1986
identifier other%28asce%290733-9445%281986%29112%3A4%28800%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/29768
description abstractIn current practice, stresses from elastic analysis are used to design reinforcement in concrete shells based on pointwise limit state behavior. This practice may be justified in view of the lower bound theorem of plasticity and the fact that elastic stresses are equilibrium stresses. Reinforced concrete, however, is not a perfectly plastic material, and the lower bound theorem cannot be strictly applied. To verify the adequacy of current practice, therefore, an analytical program was undertaken at North Carolina State Univ. A finite element computer program, which accounts for cracking of concrete and yielding of reinforcement, and that incorporates a cracking model consistent with the limit state design equations, was developed. The program was used to analyze various plane stress and shell problems. Many cases of hyperbolic paraboloid shells were also studied and are reported in this paper. It is shown that in all the saddle shell cases analyzed, the calculated ultimate capacity exceeded the design ultimate capacity. This proves the adequacy of the current practice at least for the saddle shells studied. Other conclusions of the parametric studies performed are also presented.
publisherAmerican Society of Civil Engineers
titleMembrane Reinforcement in Saddle Shells: Design versus Ultimate Behavior
typeJournal Paper
journal volume112
journal issue4
journal titleJournal of Structural Engineering
identifier doi10.1061/(ASCE)0733-9445(1986)112:4(800)
treeJournal of Structural Engineering:;1986:;Volume ( 112 ):;issue: 004
contenttypeFulltext


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