Phase-Field Modeling of Fracture Under Compression and Confinement in Anisotropic Geomaterials

IF 3.4 2区 工程技术 Q2 ENGINEERING, GEOLOGICAL
Maryam Hakimzadeh, Carlos Mora-Corral, Noel Walkington, Giuseppe Buscarnera, Kaushik Dayal
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Abstract

Strongly anisotropic geomaterials, such as layered shales, have been observed to undergo fracture under compressive loading. This paper applies a phase-field fracture model to study this fracture process. While phase-field fracture models have several advantages—primarily that the fracture path is not predetermined but arises naturally from the evolution of a smooth non-singular damage field—they provide unphysical predictions when the stress state is complex and includes compression that can cause crack faces to contact.

Building on a recently developed phase-field model that accounts for compressive traction across the crack face, this paper extends the model to the setting of anisotropic fracture. The key features of the model include the following: (1) a homogenized anisotropic elastic response and strongly anisotropic model for the work to fracture; (2) an effective damage response that accounts consistently for compressive traction across the crack face, that is derived from the anisotropic elastic response; (3) a regularized crack normal field that overcomes the shortcomings of the isotropic setting, and enables the correct crack response, both across and transverse to the crack face.

To test the model, we first compare the predictions to phase-field fracture evolution calculations in a fully resolved layered specimen with spatial inhomogeneity, and show that it captures the overall patterns of crack growth. We then apply the model to previously reported experimental observations of fracture evolution in laboratory specimens of shales under compression with confinement, and find that it predicts well the observed crack patterns in a broad range of loading conditions. We further apply the model to predict the growth of wing cracks under compression and confinement. Prior approaches to simulate wing cracks have treated the initial cracks as an external boundary, which makes them difficult to apply to general settings. Here, the effective crack response model enables us to treat the initial crack simply as a nonsingular damaged zone within the computational domain, thereby allowing for easy and general computations.

Abstract Image

各向异性土工材料压缩和约束下的断裂相场建模
强各向异性的地质材料,如层状页岩,已经被观察到在压缩载荷下发生破裂。本文采用相场断裂模型对该断裂过程进行了研究。虽然相场断裂模型有几个优点,主要是断裂路径不是预先确定的,而是从光滑的非奇异损伤场的演变中自然产生的,但当应力状态复杂且包括可能导致裂纹面接触的压缩时,它们提供了非物理预测。基于最近建立的考虑裂缝面压缩牵引力的相场模型,本文将该模型扩展到各向异性裂缝的设置。该模型的主要特征包括:(1)均质各向异性弹性响应和强各向异性断裂模型;(2)由各向异性弹性响应导出的有效损伤响应,该响应一致地考虑了整个裂纹面的压缩牵引;(3)正则化的裂缝法向场,克服了各向同性设置的缺点,实现了正确的裂缝响应,包括裂缝面的横向和横向。为了验证该模型,我们首先将预测结果与具有空间非均匀性的完全分辨层状试样的相场断裂演化计算结果进行了比较,结果表明该模型能够捕捉到裂纹扩展的整体模式。然后,我们将该模型应用于先前报道的页岩实验室试样在压缩约束下的裂缝演化实验观察,并发现它很好地预测了在广泛的加载条件下观察到的裂缝模式。我们进一步应用该模型来预测机翼在压缩和约束条件下裂纹的扩展。先前模拟机翼裂纹的方法将初始裂纹视为外部边界,这使得它们难以应用于一般设置。在这里,有效的裂纹响应模型使我们能够将初始裂纹简单地视为计算域中的非奇异损伤区,从而使计算变得简单和通用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
6.40
自引率
12.50%
发文量
160
审稿时长
9 months
期刊介绍: The journal welcomes manuscripts that substantially contribute to the understanding of the complex mechanical behaviour of geomaterials (soils, rocks, concrete, ice, snow, and powders), through innovative experimental techniques, and/or through the development of novel numerical or hybrid experimental/numerical modelling concepts in geomechanics. Topics of interest include instabilities and localization, interface and surface phenomena, fracture and failure, multi-physics and other time-dependent phenomena, micromechanics and multi-scale methods, and inverse analysis and stochastic methods. Papers related to energy and environmental issues are particularly welcome. The illustration of the proposed methods and techniques to engineering problems is encouraged. However, manuscripts dealing with applications of existing methods, or proposing incremental improvements to existing methods – in particular marginal extensions of existing analytical solutions or numerical methods – will not be considered for review.
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