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Microseismic Monitoring and Geomechanical Modelling of CO2 - bris

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3.2. INVERSION METHOD<br />

the additional compliance approach <strong>of</strong> Schoenberg <strong>and</strong> Sayers (1995), where the compliance <strong>of</strong> the<br />

fractures, ∆S, is added to the rock frame compliance, S r , to give the overall compliance,<br />

S = S r + ∆S. (3.1)<br />

Symmetry arguments reduce the number <strong>of</strong> independent terms in the 3×3×3×3 stiffness tensor from<br />

81 to 21 components. To simplify notation, the Voigt system can be used to contract C into a 6×6<br />

matrix, where the i, j <strong>and</strong> k, l subscripts <strong>of</strong> the 3×3×3×3 tensor are mapped to m <strong>and</strong> n following<br />

the convention<br />

ij or kl 11 22 33 23 = 32 13 = 31 12 = 21<br />

↓ ↓ ↓ ↓ ↓ ↓ ↓ .<br />

m or n 1 2 3 4 5 6<br />

The rock frame compliance S r can be anisotropic if horizontal layering is present. Based on<br />

previous estimates <strong>of</strong> sedimentary fabric anisotropy in siliclastic rocks (Kendall et al., 2007) I consider<br />

the rock fabric to have VTI symmetry. For such a system, the frame compliance tensor (in Voigt<br />

notation) is given by<br />

⎛<br />

C11 r (C11 r − 2C66) r C13 r 0 0 0<br />

(C 11 r − 2C66) r C11 r C13 r 0 0 0<br />

S r C13 r C13 r C33 r 0 0 0<br />

=<br />

0 0 0 C44 r 0 0<br />

⎜<br />

⎝ 0 0 0 0 C44 r 0<br />

0 0 0 0 0 C r 66<br />

⎞<br />

⎟<br />

⎠<br />

−1<br />

(3.2)<br />

. (3.3)<br />

The strength <strong>of</strong> the shear wave anisotropy caused by the VTI system is given by Thomsen’s (1986) γ<br />

<strong>and</strong> δ parameters, defined as<br />

<strong>and</strong><br />

γ = Cr 66 − C r 44<br />

2C r 44<br />

(3.4)<br />

δ = (Cr 13 + C r 44) 2 − (C r 33 − C r 44) 2<br />

2C r 33 (Cr 33 − Cr 44 ) . (3.5)<br />

The additional compliance introduced by a set <strong>of</strong> vertical, aligned fractures in a VTI medium with<br />

normals parallel to the x 1 axis (n = [1, 0, 0]) is given by Grechka (2007) as<br />

⎛<br />

⎞<br />

B N 0 0 0 0 0<br />

0 0 0 0 0 0<br />

0 0 0 0 0 0<br />

∆S =<br />

. (3.6)<br />

0 0 0 0 0 0<br />

⎜<br />

⎟<br />

⎝ 0 0 0 0 B T v 0 ⎠<br />

0 0 0 0 0 B T h<br />

B N<br />

is the normal compliance <strong>of</strong> the fracture, <strong>and</strong> B T h <strong>and</strong> B T v are the shear compliances in the<br />

vertical <strong>and</strong> horizontal planes. Having computed the stiffness tensor for fractures aligned in the x 2 :x 3<br />

plane I rotate this tensor to give the stiffness tensor for fractures with the desired strike. B T h <strong>and</strong><br />

29

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