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Finite strain plasticity, the stress condition and a complete shell model

机译:有限应变可塑性,应力条件和完整的壳模型

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The null stress (s 33 = 0) and incompressibility (J = 1) conditions in finite strain elasto-plastic shell analysis are studied in closed-form and implemented with a variant of the combined control by Ritto-Corrêa and Camotim. Coupling between constitutive laws and shell kinematics results from the satisfaction of either of the conditions; nonlocality results from the coupling. We prove that the conditions are, in general, incompatible. A new thickness-deformable is studied in terms of kinematics and strong-ellipticity. The affected continuum laws are derived and, in the discrete form, it is shown that thickness degrees-of-freedom and enhanced strains are avoided: a mixed displacement-shear strain shell element is used. Both hyperelastic and elasto-plastic constitutive laws are tested. Elasto-plasticity follows Lee’s decomposition and direct smoothing of the complementarity condition. A smooth root finder is employed to solve the resulting algebraic problem. Besides closed-form examples, numerical examples consisting of classical and newly proposed benchmarks are solved. Keywords Kinematic constraints - Variable thickness - Shells - Combined constitutive control - Finite strain plasticity - Complementarity smoothing - Mixed method J. A. C. Martins: deceased.
机译:有限应变弹塑性壳体分析中的零应力(s 33 = 0)和不可压缩性(J = 1)条件以封闭形式进行研究,并通过Ritto- Corrêa和Camotim。本构定律和壳运动学之间的耦合是由以下两个条件之一满足而产生的:非局部性是由耦合引起的。我们证明这些条件通常是不相容的。从运动学和强椭圆率方面研究了一种新的可变形厚度。推导了受影响的连续定律,并以离散形式表明避免了厚度自由度和应变增加:使用了混合位移-剪切应变壳单元。超弹性和弹塑性本构律都经过测试。弹性可塑性遵循李的分解和互补条件的直接平滑。使用光滑的寻根器来解决由此产生的代数问题。除了封闭形式的示例,还解决了由经典基准和新提出的基准组成的数值示例。运动学约束-可变厚度-壳体-组合本构控制-有限应变可塑性-互补平滑-混合方法J.A.C. Martins:已故。

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