Modeling of the stress–strain responses and deformation patterns of superelastic NiTi tubes subjected to biaxial loadings

Q3 Earth and Planetary Sciences Aerospace Systems Pub Date : 2024-01-04 DOI:10.1007/s42401-023-00266-x
Mingxun Wu, Dongjie Jiang
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Abstract

Nearly equiatomic NiTi shape memory alloy exhibits superelasticity, i.e., it can be strained up to ~ 7% and recover completely upon unloading, and consequently, the stress–strain response forms a closed hysteresis. The mechanical behavior of superelastic NiTi is characterized by significant tension–compression asymmetry, which leads to complexity in the stress–strain responses and deformation patterns of thin-walled superelastic NiTi tubes loaded by axial force and internal pressure simultaneously. In the reported biaxial experiments, the NiTi tube exhibits hardening responses and essentially homogeneous deformation in a neighborhood of equibiaxiality. In other cases, its stress–strain responses trace stress plateaus associated with localized deformation patterns, and the level of plateaus, magnitude of transformation strains, and orientation of the localization bands are strongly dependent on the axial-to-hoop stress ratio. In this paper, finite element modeling is performed to analyze numerically the mechanical response of biaxially loaded superelastic NiTi tube. A numerical feedback control scheme is developed to maintain the stress ratio to follow the target value. The simulations reproduce successfully the observed phenomena in the experiments, such as the localization of helical bands, the variation of band angles with stress ratio, as well as the hardening and uniform deformation near the state of equibiaxial stress. In addition, the variation of axial and hoop stress–strain responses with different stress ratios are also studied, which are reasonably close to the experimental ones. The presented work demonstrates the validity of the developed finite element analysis framework and paves the way for analysis of superelastic shape memory alloy structures under multiaxial loading.

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受双轴载荷作用的超弹性镍钛管的应力应变响应和变形模式建模
近等原子镍钛形状记忆合金表现出超弹性,即其应变可高达约 7%,卸载后可完全恢复,因此应力-应变响应形成闭合滞后。超弹性镍钛的力学行为具有明显的拉伸-压缩不对称特征,这导致同时承受轴向力和内压力的薄壁超弹性镍钛管的应力-应变响应和变形模式非常复杂。在报告的双轴实验中,镍钛管在等轴附近表现出硬化反应和基本均匀的变形。在其他情况下,其应力-应变响应会出现与局部变形模式相关的应力高原,而高原的水平、转变应变的大小和局部带的方向与轴向-环向应力比密切相关。本文通过有限元建模对双轴加载超弹性镍钛管的机械响应进行了数值分析。为使应力比保持在目标值,开发了一种数值反馈控制方案。模拟结果成功再现了实验中观察到的现象,如螺旋带的局部化、带角随应力比的变化,以及等轴应力状态附近的硬化和均匀变形。此外,还研究了轴向和环向应力-应变响应随不同应力比的变化,结果与实验结果相当接近。本研究成果证明了所开发的有限元分析框架的有效性,并为分析多轴载荷下的超弹性形状记忆合金结构铺平了道路。
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来源期刊
Aerospace Systems
Aerospace Systems Social Sciences-Social Sciences (miscellaneous)
CiteScore
1.80
自引率
0.00%
发文量
53
期刊介绍: Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion
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