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Buckling of cylindrical shell panels in ANSYS

Authors: D. Petrov; A. Semenov;

Buckling of cylindrical shell panels in ANSYS

Abstract

In this paper, the authors test a method of studying the stability and stress-strain state of a cylindrical shell structure under various loads in the ANSYS Mechanical APDL 19.2 software package. The analyses are performed using the arc-length method. Shell 181 is chosen as an element type, which makes it possible to account for large strains during the analyses. The shells have fixed-pin joints on two sides and a free edge on the other two sides. A concentrated force and a uniformly distributed load are considered as load cases. Normal displacement vs. load graphs are obtained for all options of the structures considered; the values are calculated with account for geometric nonlinearity. Buckling load values are obtained for various options of structures with a uniformly distributed load, the other structures remain stable. A significant difference in critical values as compared to the linear analysis indicates the need for taking into account geometric nonlinearity.

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
1
Average
Average
Average
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