首页> 外文期刊>Tectonophysics: International Journal of Geotectonics and the Geology and Physics of the Interior of the Earth >FEM analysis of deformation localization mechanisms in a 3-D fractured medium under rotating compressive stress orientations
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FEM analysis of deformation localization mechanisms in a 3-D fractured medium under rotating compressive stress orientations

机译:旋转压应力作用下3-D压裂介质变形局部化机制的有限元分析

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摘要

Stress distributions and deformation patterns in a medium with a pre-existing fracture set are analyzed as a function of the remote compressive stress orientation (σ_H) using finite element models with increasingly complex fracture configurations. Slip along the fractures causes deformation localization at the tips as wing cracks or shear zones. The deformation intensity is proportional to the amount of slip, attaining a peak value for α=45° (α: angle between the fracture strike and σ_H) and slip is linearly proportional with fracture length. Wing cracks develop for high deformation intensities for 30°<α<60°, whereas primary plastic shear zones develop for low deformation intensities. Additionally, two types of secondary shear zones develop for α<30° and α>60°, with constant angles of 135° and -60° with σ_H, respectively.Mechanical interaction between fractures in a fracture zone, quantified as change in slip compared to an isolated fracture, decreases with increasing fracture separation. Fracture underlap elongates the fracture length and therefore increases the amount of slip, while fracture overlap exhibits the opposite effect. Fracture slip decreases with an increasing amount of directly adjacent fractures. Mechanical interaction becomes negligible for fracture configurations with spacing-to-length and spacing-to-overlap ratios exceeding 0.5 and that in this case fractures are decoupled.Independent of the pre-existing fracture configuration, the development of a secondary systematic fracture set driven by a remote stress rotation is dominated by σ_H; development of wing cracks or shear zones is restricted to the fracture tips. Blocks with tapered geometries are present in models with a variable fracture strike, where the maximum principal stress (σ_1, applying the geological convention that compressive stresses are positive) trajectories consistently deviate from σ_H; the presence of two systematic σ_1 trajectory orientations suggests that two types of secondary features could develop in one re-activation phase.
机译:使用具有日益复杂的裂缝构造的有限元模型,分析具有预先裂缝集的介质中的应力分布和变形模式,作为远程​​压缩应力方向(σ_H)的函数。沿裂缝滑动会导致尖端处的变形局部化,如机翼裂纹或剪切区。变形强度与滑移量成正比,达到α= 45°的峰值(α:断裂冲击与σ_H之间的夹角),滑移与断裂长度成线性比例。翼形裂纹在30°<α<60°时具有较高的变形强度,而初级塑性剪切区则具有较低的变形强度。此外,α<30°和α> 60°分别形成了两种类型的次级剪切带,分别与σ_H的恒定夹角为135°和-60°。到孤立的裂缝,随着裂缝间距的增加而减小。断裂下重叠延长了断裂长度,因此增加了滑移量,而断裂重叠表现出相反的效果。随着直接相邻裂缝数量的增加,裂缝滑移减小。对于间距与长度之比和间距与重叠率之比超过0.5的裂缝构型,机械相互作用变得微不足道,在这种情况下,裂缝是解耦的。远程应力旋转由σ_H控制;机翼裂纹或剪切区的发展仅限于断裂尖端。在具有可变断裂走向的模型中存在具有锥形几何形状的块,其中最大主应力(σ_1,应用压应力为正的地质惯例)轨迹始终偏离σ_H;两个系统的σ_1轨迹方向的存在表明,在一个重新激活阶段可能会形成两种类型的辅助特征。

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