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structural geology, propagation mechanics and - Stanford School of ...

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2005). It consists <strong>of</strong> a long (infinite in the x-direction) layer <strong>of</strong> material <strong>of</strong> thickness h (in<br />

the y-direction). The layer contains a long (semi-infinite) CB which attains a fixed<br />

thickness ξ h far behind the b<strong>and</strong> edge. Both the layer <strong>and</strong> the b<strong>and</strong> are uniform in z-<br />

direction (orthogonal to the xy-plane <strong>of</strong> Figure 3.2), at least over distances much larger<br />

than h. The layer boundaries are then displaced toward each other a total distance ∆. The<br />

geometry constrains all displacements <strong>and</strong> strains to be uniaxial in the vertical (y)<br />

direction. Because the configuration is self-similar (translationally invariant in the x-<br />

direction), <strong>propagation</strong> <strong>of</strong> the CB a unit distance in the x-direction must reduce the strain<br />

energy in a vertical slice (perpendicular to the xy-plane) far ahead <strong>of</strong> the b<strong>and</strong> edge to that<br />

<strong>of</strong> a vertical slice far behind the b<strong>and</strong> edge. Because displacement is fixed on the<br />

boundaries <strong>of</strong> the sample, this difference in strain energy exactly equals the energy<br />

released per unit area swept out by <strong>propagation</strong> <strong>of</strong> the CB a unit distance.<br />

Far ahead <strong>of</strong> the b<strong>and</strong>, the vertical strain is uniform <strong>and</strong> equal to ∆/ h . If the material<br />

is assumed to be elastic, then the vertical stress is M(∆/h) (horizontal stresses exist to<br />

enforce zero strain in these directions), where M is the modulus governing one-<br />

dimensional strain. For an isotropic material with shear modulus G <strong>and</strong> Poisson’s ratio<br />

ν , M = 2 G(1 − ν ) / (1− 2 ν ) . The strain energy per unit area <strong>of</strong> a vertical slice far ahead <strong>of</strong><br />

the CB is<br />

2<br />

+ 1 ⎛∆⎞ W = Mh⎜ ⎟ . (2)<br />

2 ⎝ h ⎠<br />

Far behind the b<strong>and</strong> edge, where the CB thickness is ξ h , the strain is uniform both<br />

inside ( ε b<strong>and</strong> ) <strong>and</strong> outside ( ε out ) the b<strong>and</strong>. The values are different but must be compatible<br />

with the total displacement <strong>of</strong> the boundary, given by<br />

ξhε + (1 − ξ) hε<br />

=∆. (3)<br />

b<strong>and</strong> out<br />

The stress outside the CB is given by σ out Mε<br />

out<br />

= . The material inside the CB is also<br />

assumed to be elastic, but with a different modulus M b , <strong>and</strong> to have undergone an<br />

p<br />

inelastic, vertical compactive strain ε . Hence, the stress is given by<br />

σ = M ε −ε<br />

⎛<br />

b<strong>and</strong> b ⎜<br />

⎝ b<strong>and</strong><br />

p ⎞<br />

⎟<br />

⎠<br />

. (4)<br />

80

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