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NON-LOCAL PLASTIC-DAMAGE MODEL FOR FAILURE ANALYSIS OFSHEET-METALS

机译:板料失效分析的非局部塑性损伤模型

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A ductile damage model which takes account of void shape effect and anisotropy of the matrix material is integrated into an explicit finite element framework to predict the damage evolution which occurs under crash or stamping process.The void coalescence failure mechanism by internal necking is considered by using a modified Thomason's plastic limit-load model.A 3D.Analysis of a unit cube (RVE) containing an ellipsoidal void and rigid inclusion has been carried out to calibrate the coalescence model.The pathological mesh dependence has been overcome by a non-local approach where the Laplacians of the effective plastic strain and of the porosity are incorporated.The implicit gradient formulation constitutes an additional partialdifferential equation of the Helmholtz type which is solved separately here by a boundary element method (BEM).The presented formulation is applied to determine the Forming Limit Diagrams (FLD) of an aluminum alloy of a 5182 type.The effectiveness of the numerical predictions is verified carrying out a set of experimental tests with flat-headed and hemispherical punches and D.I.C.strain measurements.
机译:考虑到空洞形状效应和基体材料各向异性的延性破坏模型被集成到一个显式的有限元框架中,以预测在碰撞或冲压过程中发生的破坏演化。修改后的Thomason塑性极限载荷模型.3D。对包含椭圆形空隙和刚性夹杂物的单位立方体(RVE)进行了分析,以校准聚结模型。通过非局部方法克服了病理网格依赖性隐式梯度公式构成了Helmholtz型的附加偏微分方程,可通过边界元法(BEM)单独求解,并采用所提出的公式来确定拉普拉斯算子的有效塑性应变和孔隙率。 5182型铝合金的成形极限图(FLD)数字的有效性通过平头和半球形冲头以及D.I.C.应变测量进行的一系列实验测试,验证了所有预测。

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