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A Finite Strain Constitutive Model for Martensitic Transformation in Shape Memory Alloys Based on Logarithmic Strain

机译:基于对数应变的形状记忆合金马氏体转变的有限应变本构模型

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Shape Memory Alloys (SMAs) are materials with the ability to recover apparently permanent deformation under specific thermomechanical loading and are thus desirable in various fields such as aerospace and automobile, among others. Most constitutive models for SMAs in the literature are developed based on the assumption of infinitesimal strain. However, such an assumption may not be proper in the presence of geometric discontinuities, such as cracks, and repeated cycling loading that has been reported to induce irrecoverable strains up to 20% due to transformation induced plasticity. In addition to finite strains, SMA-based devices may also undergo finite rotations. Thus, it is indispensable to develop a constitutive model based on finite strain to provide for accurate predictions of these actuators response. A three-dimensional phenomenological constitutive model for SMAs considering finite strains and finite rotations is proposed in this work. This model utilizes the logarithmic strain, or called natural strain, as a finite strain measure which is the only strain measure whose logarithmic rate in a corotating material frame is equal to the rate of deformation tensor. The proposed constitutive model is motivated by the earlier work of Lagoudas and coworkers based on the infinitesimal strain assumption. In the proposed model, the martensitic volume fraction and the second-order logarithmic transformation strain tensor are chosen as the internal state variables associated with the inelastic transformation process. Numerical simulations considering basic SMAs component geometries such as a bar, a beam and a torque tube are performed to test the capabilities of proposed model under both mechanically and thermally induced phase transformation. For numerical examples in which the SMA components exhibits finite strains along with finite rotations, discrepancies are observed between the responses predicted by the present model and its infinitesimal counterpart. Also, the spurious accumulated residual stress observed in infinitesimal strain model is eliminated by proposed model. This shows that the infinitesimal strain assumption is not applicable in such cases and the proposed model considering large strains and rotations is needed to provide accurate predictions. The presented model formulation will be extended in future work for the incorporation of transformation-induced plasticity.
机译:形状记忆合金(SMA)是具有在特定的热机械载荷下能够恢复表观永久变形的能力的材料,因此在航空航天和汽车等各个领域都是理想的。文献中针对SMA的大多数本构模型都是基于无穷大应变的假设而开发的。但是,这种假设在存在几何不连续性(例如裂缝)和重复循环载荷的情况下可能不合适,据报道,由于循环诱导的可塑性,反复循环载荷会诱导高达20%的不可恢复应变。除了有限的应变,基于SMA的设备也可能会受到有限的旋转。因此,开发基于有限应变的本构模型以提供这些致动器响应的准确预测是必不可少的。在这项工作中,提出了一种考虑有限应变和有限旋转的三维SMA现象学本构模型。该模型将对数应变(即自然应变)用作有限应变度量,这是唯一在同向旋转材料框架中对数率等于变形张量率的应变度量。提出的本构模型是由Lagoudas和同事基于无穷小应​​变假设的早期工作所激发的。在提出的模型中,选择马氏体体积分数和二阶对数转变应变张量作为与非弹性转变过程相关的内部状态变量。进行了考虑基本SMAs部件几何形状(例如杆,梁和扭矩管)的数值模拟,以测试所提出的模型在机械和热致相变下的性能。对于其中SMA分量随有限旋转显示有限应变的数值示例,在本模型预测的响应与其无穷小对应之间观察到差异。此外,通过所提出的模型消除了在无限小应变模型中观察到的虚假累积残余应力。这表明无穷小应变假设不适用于此类情况,并且需要考虑大应变和旋转的建议模型才能提供准确的预测。提出的模型公式将在未来的工作中扩展,以纳入由转换引起的可塑性。

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