FEM analysis of deformation localization mechanisms in a 3-D fractured medium under rotating compressive stress orientations
Publication date
2013
Authors
Strijker, G.
Beekman, F.
Bertotti, G.
Luthi, S.M.
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Advisors
Supervisors
Document Type
Article
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(c) UU Universiteit Utrecht, 2013
Abstract
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 (σH) 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 σH) and slip is linearly proportional with fracture
length. Wing cracks develop for high deformation intensities for 30° b α b 60°, whereas primary plastic
shear zones develop for low deformation intensities. Additionally, two types of secondary shear zones develop
for α b 30° and α > 60°, with constant angles of 135° and −60° with σH, 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 σH; 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 (σ1, applying the geological convention that compressive stresses
are positive) trajectories consistently deviate from σH; the presence of two systematic σ1 trajectory orientations
suggests that two types of secondary features could develop in one re-activation phase.
Keywords
Finite element method, Fracture, Re-activation, Wing crack, Shear zone, Mechanical interaction