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155 Faults and fractures at depth<br />

a. b.<br />

Active shear planes<br />

Mode 2 and Mode 3<br />

t<br />

Mode 1<br />

m = 1.0<br />

2b 3<br />

m = 0.6<br />

2b 1<br />

s 3 s 2 s 1<br />

P<br />

S n<br />

S 1<br />

b 3<br />

b 1<br />

S 3<br />

S 2<br />

P<br />

FAULT<br />

Figure 5.9. Representation of the shear and effective normal stress on an arbitrarily oriented fault<br />

can be accomplished with a three-dimensional Mohr circle (a). Although the exact position of<br />

point P can be determined with angles β 1 and β 3 measured between the fault normal and S 1<br />

and S 3 directions (b) utilizing the graphical reconstruction shown, it is typical to calculate this<br />

mathematically (see text) and utilize the three-dimensional Mohr diagram for representation of<br />

the data.<br />

location of P graphically, one utilizes the angles 2β 1 and 2β 3 to find points on the two<br />

small circles, and by constructing arcs drawn from the center of the other Mohr circle,<br />

Pisdetermined as the intersection of the two arcs. It is obvious that a Mode I plane<br />

(normal to the least principal stress) plots at the position of σ 3 in the Mohr diagram.<br />

Of course, it is not necessary these days to use graphical techniques alone for determining<br />

the shear and effective normal stress on arbitrarily oriented planes, but threedimensional<br />

Mohr diagrams remain quite useful for representing fault data, as will be<br />

illustrated in the chapters that follow.<br />

There are two common methods for calculating the magnitude of shear and normal<br />

stress on an arbitrarily oriented plane. The first technique defines the shear and normal<br />

stress in terms of the effective principal stresses and the orientation of the fault plane<br />

to the stress field. The shear and effective normal stresses are given by<br />

τ = a 11 a 12 σ 1 + a 12 a 22 σ 2 + a 13 a 23 σ 3 (5.7)<br />

σ n = a11 2 σ 1 + a12 2 σ 2 + a13 2 σ 3 (5.8)<br />

where a ij are the direction cosines (Jaeger and Cook 1971):<br />

⎡<br />

⎤<br />

cos γ cos λ cos γ sin λ −sin γ<br />

⎢<br />

⎥<br />

A = ⎣ −sin λ cos λ 0 ⎦ (5.9)<br />

sin γ cos λ sin γ sin λ cos γ<br />

where γ is the angle between the fault normal and S 3 , and λ is the angle between the<br />

projection of the fault strike direction and S 1 in the S 1 –S 2 plane.

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