Abstract
Strain-hardening behavior for plane stress problems is modeled by a panel with n layers, the first (n - 1) layers are elastic-perfectly-plastic under Mises-Hencky condition, each with different yield stress, and the n-th layer is elastic. Equivalent incremental stress-strain relations for the panel can be obtained. The resulting uniaxial stress-strain curve contains n segments. Those segments in the plastic range are not straight lines.
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Communicated by S. N. Atluri, April 28, 1986
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Pian, T.H.H. Mechanical sublayer model for elastic-plastic analyses. Computational Mechanics 2, 26–30 (1987). https://doi.org/10.1007/BF00282041
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DOI: https://doi.org/10.1007/BF00282041