structural geology, propagation mechanics and - Stanford School of ...
structural geology, propagation mechanics and - Stanford School of ...
structural geology, propagation mechanics and - Stanford School of ...
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σ<br />
b<br />
33<br />
1+<br />
ν b =<br />
2<br />
G<br />
G<br />
b<br />
s<br />
( 1−ν<br />
)<br />
b<br />
⎧<br />
⎨<br />
⎩<br />
∞ ∞ ( σ −σ )<br />
22<br />
2<br />
( 1−ν<br />
s )<br />
( 1+<br />
ν )<br />
33<br />
s<br />
G<br />
G<br />
b<br />
s<br />
∞ ∞ ( σ + σ )<br />
22<br />
33<br />
∞ ⎡<br />
+ σ11⎢<br />
⎣<br />
2ν<br />
b<br />
G<br />
−<br />
( 1+<br />
ν ) G ( 1+<br />
ν )<br />
b<br />
b<br />
s<br />
2ν<br />
s<br />
s<br />
⎤⎫<br />
⎥⎬<br />
−<br />
⎦⎭<br />
where the subscripts “b” <strong>and</strong> “s” denote the elastic parameters <strong>of</strong> the b<strong>and</strong> <strong>and</strong><br />
surrounding s<strong>and</strong>stone, respectively.<br />
The state <strong>of</strong> stress at the point adjacent to <strong>and</strong> immediately outside the tip <strong>of</strong> the<br />
model b<strong>and</strong> along the x2-axis can now be obtained from the conditions <strong>of</strong> displacement<br />
<strong>and</strong> traction continuity at the interface:<br />
σ = σ<br />
(5a)<br />
t<br />
22<br />
t<br />
11<br />
b<br />
11<br />
b<br />
22<br />
t b<br />
ε = ε , ε = ε<br />
(5b)<br />
33<br />
33<br />
where the superscript “t” refers to the values just outside the tip. In the second equation<br />
<strong>of</strong> (5b), ε33 t can be replaced by ε33 ∞ from the second equation <strong>of</strong> (1b). Again, the elasticity<br />
relations can be used to eliminate the elastic strains <strong>and</strong> yield expressions for the stresses<br />
at the tip <strong>of</strong> the b<strong>and</strong> in terms <strong>of</strong> the uniform stresses inside, the elastic constants <strong>and</strong> the<br />
nonzero plastic strain component ε11 p :<br />
σ<br />
G<br />
ν<br />
⎛ G<br />
⎜ −<br />
⎝<br />
⎞<br />
⎟<br />
⎠<br />
G<br />
ν −ν<br />
t s b s b s s b s b<br />
s p<br />
11 = σ 11 + σ 22 1 σ kk<br />
ε11<br />
Gb<br />
( 1 ν s ) ⎜ G ⎟<br />
+<br />
+<br />
(6a)<br />
−<br />
b Gb<br />
( 1−ν<br />
s )( 1+<br />
ν b ) ( 1−ν<br />
s )<br />
σ = σ<br />
(6b)<br />
σ<br />
t<br />
22<br />
G<br />
b<br />
22<br />
ν<br />
⎛ G<br />
⎜ −<br />
⎝<br />
⎞<br />
⎟<br />
⎠<br />
G<br />
ν −ν<br />
t s b s b s s b s b<br />
s p<br />
33 = σ 33 + σ 22 1 σ kk<br />
ν sε11<br />
Gb<br />
( 1 ν s ) ⎜ G ⎟<br />
+<br />
+<br />
(6c)<br />
−<br />
b Gb<br />
( 1−ν<br />
s )( 1+<br />
ν b ) ( 1−ν<br />
s )<br />
By substituting (4) into (6), expressions for the stresses at the tip in terms <strong>of</strong> the<br />
remote values also can be derived. It can be seen from (6) that, for given values <strong>of</strong> the<br />
elastic parameters <strong>and</strong> remote stresses, σ11 t <strong>and</strong> σ33 t are linear functions <strong>of</strong> ε11 p , with<br />
slopes <strong>of</strong> 2Gs/(1-νs) <strong>and</strong> [2Gs/(1-νs)] νs, respectively, while σ22 t remains constant. In fact,<br />
for ε11 p > 10 -3 <strong>and</strong> any realistic range <strong>of</strong> elastic parameters <strong>and</strong> remote stresses, the final<br />
63<br />
2G<br />
2G<br />
(4c)