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A general approximate technique for the finite element shakedown and limit analysis of axisymmetrical shells. Part 1: Theory and fundamental relations
Author(s) -
Franco Jose Ricardo Queiroz,
Ponter Alan R. S.
Publication year - 1997
Publication title -
international journal for numerical methods in engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.421
H-Index - 168
eISSN - 1097-0207
pISSN - 0029-5981
DOI - 10.1002/(sici)1097-0207(19971015)40:19<3495::aid-nme222>3.0.co;2-u
Subject(s) - shakedown , finite element method , limit analysis , mathematics , discretization , piecewise linear function , shell (structure) , mathematical analysis , piecewise , curvature , displacement field , limit (mathematics) , displacement (psychology) , geometry , upper and lower bounds , structural engineering , engineering , psychology , civil engineering , psychotherapist
This paper describes the theory and the fundamental relations for the development of a displacement formulation for the finite element shakedown and limit analysis of axi‐symmetrical shells. The material is assumed to be elastic–perfectly plastic. The technique is developed based upon an upper bound approach using a reformulated kinematic shakedown theorem for a shell with piecewise linear yield conditions. The solution of the problem is obtained by discretizing the shell into finite elements. A consistent relationship between the kinematically admissible velocity fields and the pure plastic strain rate fields during collapse needs to be enforced. Such requirement is satisfied by using the theory of conjugate approximations to minimize the residual of the two independent descriptions of the plastic strain increments. The discretized problem is then reduced to a minimization problem and solved by linear programming. The class of displacement fields chosen assumes plastic hinge lines forming at nodal points and only meridional and circumferential plastic strains occurring within the elements with no change in curvature. Examples of the application of the method are given in the accompanying paper. © 1997 John Wiley & Sons, Ltd.