地球与空间科学 · 第 3 册 · 本科一年级

University Earth and Space Sciences — Year 1

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University Earth and Space Sciences — Year 1 · 本科一年级

16Stress, Strain and Rheology

In the 1960s, waste fluid pumped down a disposal well at the Rocky Mountain Arsenal, near Denver, spread through fractured crystalline basement between 3.7 km3.7\,\mathrm{km} and 7.0 km7.0\,\mathrm{km} below the surface, and earthquakes followed. They stayed inside the part of the rock where the fluid pressure had risen by more than about 3.2 MPa3.2\,\mathrm{MPa}.

Half a century later the same thing happened on a larger scale in Oklahoma, where salty water brought up with oil and gas is pumped back underground. In and around the state, the earthquakes of magnitude 3 or more numbered one to five a year from 2005 to 2008, then 2020 in 2009, 585585 in 2014 and 888888 in 2015, more than two a day; shocks of magnitude 5.7 and 5.8 shook Prague, in 2011, and Pawnee, in 2016. Four high-volume disposal wells alone could account for a fifth of the earthquakes of the central United States, and set off some more than 30 km30\,\mathrm{km} away.

The water pushed nothing aside; it only raised the pressure of the fluid in the pores of the rock. Why should that make a fault slip? The answer needs three ideas, which are the subject of this chapter: the stress on a plane inside a rock, the condition under which the plane gives way, and the fact that the pressure of the pore fluid counts against the force pressing the two sides together. With them, and with a law of creep for hot rock, we can draw the strength of the whole lithosphere against depth.

You already know

A force spread over a surface acts through its force per unit area, in pascals; the pressure in a fluid at rest grows with depth as ρgz\rho g z (physics books). A spring, and a solid in small deformations, obey Hooke’s law: the strain is proportional to the stress, with Young’s modulus as the constant; a viscous fluid resists in proportion to its rate of shear, with its viscosity as the constant. The physics books’ University Year 3 volume describes stress and strain in three dimensions with tensors; this chapter needs only two. A symmetric 2×22\times2 matrix has two real eigenvalues and two perpendicular eigenvectors (mathematics, Year 1). The geotherms of Chapter 10 give the temperature at depth; faults were met in Book 1, grade 7.

16.1 Stress in two dimensions

Cut a rock in thought along a small flat surface. The rock on one side presses on the rock on the other with a force, and the force per unit area is the traction on that surface, in the physics books’ word. Its direction is not, in general, the direction of the normal to the surface.

Definition 16.1 (Normal stress)

On a plane through a point of a rock, the force per unit area that the rock on one side exerts on the other has a component along the normal to the plane, the normal stress σn\sigma_n, and a component along the plane, the shear stress τ\tau. In the Earth sciences the normal stress is counted positive when it compresses.

The sign convention is the opposite of the engineer’s. It is chosen because nearly every stress in the solid Earth is a compression: the weight of the rock above presses on everything below it.

We work in a vertical plane, with an axis xx horizontal and an axis yy. On a plane perpendicular to xx the normal stress is σxx\sigma_{xx} and the shear stress σxy\sigma_{xy}; on a plane perpendicular to yy they are σyy\sigma_{yy} and σyx\sigma_{yx}. The two shear stresses are equal: on a small square, the shear forces on the vertical sides make a couple of moment σxya⋅a\sigma_{xy}a\cdot a for a side aa, those on the horizontal sides a couple σyxa⋅a\sigma_{yx}a\cdot a turning the other way, and the square would spin if they differed. So three numbers describe the stress at a point, and they are enough to give it on every plane.

Proposition 16.2 (Stress on an inclined plane)

Let a plane have the unit normal n⃗=(cos⁡θ,sin⁡θ)\vec n = (\cos\theta, \sin\theta), at the angle θ\theta from the axis xx, and let m⃗=(−sin⁡θ,cos⁡θ)\vec m = (-\sin\theta, \cos\theta) be the unit vector along the plane. The normal and shear stresses on it are

σn=σxxcos⁡2θ+2σxysin⁡θcos⁡θ+σyysin⁡2θ=σxx+σyy2+σxx−σyy2cos⁡2θ+σxysin⁡2θ,τ=(σyy−σxx)sin⁡θcos⁡θ+σxy(cos⁡2θ−sin⁡2θ)=−σxx−σyy2sin⁡2θ+σxycos⁡2θ,\begin{align*} \sigma_n &= \sigma_{xx}\cos^2\theta + 2\sigma_{xy}\sin\theta\cos\theta + \sigma_{yy}\sin^2\theta = \frac{\sigma_{xx}+\sigma_{yy}}{2} + \frac{\sigma_{xx}-\sigma_{yy}}{2}\cos2\theta + \sigma_{xy}\sin2\theta, \\ \tau &= (\sigma_{yy}-\sigma_{xx})\sin\theta\cos\theta + \sigma_{xy}(\cos^2\theta - \sin^2\theta) = -\frac{\sigma_{xx}-\sigma_{yy}}{2}\sin2\theta + \sigma_{xy}\cos2\theta , \end{align*}

with τ\tau counted positive along m⃗\vec m.

Proof. Cut out a small prism, as in the figure below: an inclined face of area AA with the outward normal n⃗\vec n, a vertical face of area Acos⁡θA\cos\theta and a horizontal face of area Asin⁡θA\sin\theta, per unit length in the third direction. Its weight and its inertia scale as its volume, which shrinks faster than its faces; for a small enough prism the forces on the faces must balance on their own. Compression being positive, the rock outside pushes on the vertical face with the force Acos⁡θ (σxx,σxy)A\cos\theta\,(\sigma_{xx}, \sigma_{xy}) and on the horizontal face with Asin⁡θ (σxy,σyy)A\sin\theta\,(\sigma_{xy}, \sigma_{yy}); on the inclined face it pushes with −A(σnn⃗+τm⃗)-A(\sigma_n\vec n + \tau\vec m). The sum is zero:

σnn⃗+τm⃗=cos⁡θ (σxx,σxy)+sin⁡θ (σxy,σyy).\sigma_n\vec n + \tau\vec m = \cos\theta\,(\sigma_{xx}, \sigma_{xy}) + \sin\theta\,(\sigma_{xy}, \sigma_{yy}) .

The scalar product with n⃗\vec n gives σn\sigma_n, with m⃗\vec m gives τ\tau, since n⃗⋅m⃗=0\vec n\cdot\vec m = 0. The second forms follow from cos⁡2θ=(1+cos⁡2θ)/2\cos^2\theta = (1+\cos2\theta)/2, sin⁡2θ=(1−cos⁡2θ)/2\sin^2\theta = (1-\cos2\theta)/2 and 2sin⁡θcos⁡θ=sin⁡2θ2\sin\theta\cos\theta = \sin2\theta. ∎

The balance of forces on a small triangular prism of rock. The inclined face has the area A and the unit normal n; the vertical and horizontal faces have the areas A and A. Blue: the normal forces on the two small faces; orange: the shear forces on them; red: the normal and shear forces on the inclined face. Compression is counted positive, so every normal force points into the prism.
The balance of forces on a small triangular prism of rock. The inclined face has the area AA and the unit normal n⃗\vec n; the vertical and horizontal faces have the areas Acos⁡θA\cos\theta and Asin⁡θA\sin\theta. Blue: the normal forces on the two small faces; orange: the shear forces on them; red: the normal and shear forces on the inclined face. Compression is counted positive, so every normal force points into the prism.

Theorem 16.3 (Principal stresses)

At every point of a rock there are two perpendicular planes on which the shear stress is zero. The normal stresses on them are the largest and the smallest normal stress over all planes through the point,

σ1,3=σxx+σyy2±(σxx−σyy2)2+σxy2,tan⁡2θp=2σxyσxx−σyy,\sigma_{1,3} = \frac{\sigma_{xx}+\sigma_{yy}}{2} \pm \sqrt{\Bigl(\frac{\sigma_{xx}-\sigma_{yy}}{2}\Bigr)^2 + \sigma_{xy}^2}, \qquad \tan2\theta_p = \frac{2\sigma_{xy}}{\sigma_{xx}-\sigma_{yy}},

where θp\theta_p is the angle from the axis xx to the normal of the plane that carries σ1\sigma_1.

Proof. Write c=(σxx+σyy)/2c = (\sigma_{xx}+\sigma_{yy})/2, and choose R≥0R \ge 0 and θp\theta_p with (σxx−σyy)/2=Rcos⁡2θp(\sigma_{xx}-\sigma_{yy})/2 = R\cos2\theta_p and σxy=Rsin⁡2θp\sigma_{xy} = R\sin2\theta_p; then R=((σxx−σyy)/2)2+σxy2R = \sqrt{((\sigma_{xx}-\sigma_{yy})/2)^2 + \sigma_{xy}^2} and tan⁡2θp\tan2\theta_p is as stated. The second forms of Proposition 16.2 become

σn=c+Rcos⁡(2θ−2θp),τ=−Rsin⁡(2θ−2θp).\sigma_n = c + R\cos(2\theta - 2\theta_p), \qquad \tau = -R\sin(2\theta - 2\theta_p).

The normal stress is largest, c+Rc + R, for θ=θp\theta = \theta_p, and smallest, c−Rc - R, for θ=θp+90∘\theta = \theta_p + 90{}^{\circ}; at both, τ=0\tau = 0. Note also that dσn/dθ=2τ\mathrm d\sigma_n/\mathrm d\theta = 2\tau: the normal stress is stationary exactly where the shear stress vanishes. ∎

Definition 16.4 (Principal stresses, differential stress)

The principal stresses at a point are the normal stresses σ1≥σ3\sigma_1 \ge \sigma_3 on the two planes free of shear stress, and their directions are the principal directions. In three dimensions there are three, σ1≥σ2≥σ3\sigma_1 \ge \sigma_2 \ge \sigma_3, on three perpendicular planes. The differential stress is σ1−σ3\sigma_1 - \sigma_3, and the mean stress in the plane is (σ1+σ3)/2(\sigma_1+\sigma_3)/2.

A state of stress is easiest to read in its principal directions. If we measure the angle θ\theta from the direction of σ1\sigma_1 instead of from the axis xx, the formulas lose their last terms.

Proposition 16.5 (Mohr’s circle)

On a plane whose normal makes the angle θ\theta with the direction of σ1\sigma_1,

σn=σ1+σ32+σ1−σ32cos⁡2θ,∣τ∣=σ1−σ32 ∣sin⁡2θ∣.\sigma_n = \frac{\sigma_1+\sigma_3}{2} + \frac{\sigma_1-\sigma_3}{2}\cos2\theta, \qquad |\tau| = \frac{\sigma_1-\sigma_3}{2}\,|\sin2\theta| .

As θ\theta turns, the point (σn,∣τ∣)(\sigma_n, |\tau|) runs over the upper half of the circle of centre ((σ1+σ3)/2, 0)((\sigma_1+\sigma_3)/2,\, 0) and radius (σ1−σ3)/2(\sigma_1-\sigma_3)/2, at the angle 2θ2\theta from its σ1\sigma_1 end. The largest shear stress, (σ1−σ3)/2(\sigma_1-\sigma_3)/2, acts on the planes at 45∘45{}^{\circ} to the principal directions.

Proof. In the principal axes σxx=σ1\sigma_{xx} = \sigma_1, σyy=σ3\sigma_{yy} = \sigma_3 and σxy=0\sigma_{xy} = 0, and Proposition 16.2 gives the two formulas. Then (σn−(σ1+σ3)/2)2+τ2=((σ1−σ3)/2)2(\sigma_n - (\sigma_1+\sigma_3)/2)^2 + \tau^2 = ((\sigma_1-\sigma_3)/2)^2, the equation of the circle; ∣sin⁡2θ∣|\sin2\theta| is largest for θ=45∘\theta = 45{}^{\circ}. ∎

The sign of τ\tau only says in which sense the two sides would slide, so the upper half of the circle is usually drawn alone. The construction is named after the engineer Christian Otto Mohr, who also built on it a criterion of failure, which is where we are going (Section 16.3).

Stress at depth

Definition 16.6 (Lithostatic pressure, pore-fluid pressure, effective stress)

At the depth zz, the weight of the rock above, per unit of horizontal area, is the vertical stress σv=∫0zρg dz′\sigma_v = \int_0^z\rho g\,\mathrm dz', which is ρgz\rho g z in a layer of uniform density ρ\rho. When the stress is the same in every direction and equal to it, the rock is under the lithostatic pressure. The pressure of the water, oil or gas in the pores and cracks of the rock is the pore-fluid pressure PP; it is hydrostatic, P=ρwgzP = \rho_w g z, when the pores connect to the surface. The effective stress is the stress minus the pore pressure, σ′=σ−P\sigma' = \sigma - P, on every plane; λ=P/σv\lambda = P/\sigma_v is the pore-pressure ratio.

In a crust of density 2700 kg m−32700\,\mathrm{kg}\,\mathrm{m}^{-3}, the vertical stress grows by 2700×9.81×1000=26.5 MPa2700\times9.81\times1000 = 26.5\,\mathrm{MPa} per kilometre and a hydrostatic pore pressure by 9.81 MPa9.81\,\mathrm{MPa} per kilometre: λ=1000/2700=0.37\lambda = 1000/2700 = 0.37. The pore fluid pushes the grains apart with the same pressure in every direction; it takes nothing from the shear stress, but it takes PP from every normal stress. Where the pores are sealed, by clay or salt for instance, the fluid can carry part of the weight of the rock above, and λ\lambda rises towards 1.

The stress in the crust is not lithostatic. Plates push and pull, the crust bends, mountains weigh on their roots, and the horizontal stresses differ from the vertical one. Near the surface, which carries no shear stress, one principal direction is vertical, as Chapter 17 shows: σv\sigma_v is σ1\sigma_1, σ2\sigma_2 or σ3\sigma_3, and the three cases are the three ways faults move.

16.2 Strain

Stress is a cause; strain is what the rock records. A fossil drawn out, a pebble flattened, a bed shortened into folds all measure a change of shape.

Definition 16.7 (Extension, stretch, shear strain)

A line of material of length ℓ0\ell_0 deformed to the length ℓ\ell has the extension e=(ℓ−ℓ0)/ℓ0e = (\ell - \ell_0)/\ell_0 and the stretch S=ℓ/ℓ0=1+eS = \ell/\ell_0 = 1 + e; a shortening is a negative extension, a stretch below 1. Two lines of material that were perpendicular and now make the angle 90∘−ψ90{}^{\circ} - \psi have been sheared by the angle ψ\psi, and the shear strain is γ=tan⁡ψ\gamma = \tan\psi.

A strain is homogeneous when every small region of the rock deforms in the same way. The new position x⃗′\vec x' of the point x⃗\vec x is then a linear function, x⃗′=Fx⃗\vec x' = F\vec x, with a constant 2×22\times2 matrix FF (and det⁡F>0\det F > 0, since rock does not turn inside out). Straight lines stay straight and parallel lines parallel; a square becomes a parallelogram, and a circle becomes an ellipse.

Proposition 16.8 (The strain ellipse)

Under the homogeneous strain x⃗′=Fx⃗\vec x' = F\vec x, the circle of radius 1 becomes an ellipse whose semi-axes are the square roots S1≥S2S_1 \ge S_2 of the eigenvalues of FFTFF^{\mathsf T}, along its perpendicular eigenvectors. S1S_1 and S2S_2 are the largest and smallest stretches of all lines of material, and the area is multiplied by det⁡F=S1S2\det F = S_1S_2.

Proof. The point x⃗=Fu⃗\vec x = F\vec u comes from a point u⃗\vec u of the circle, ∣u⃗∣=1|\vec u| = 1, so ∣F−1x⃗∣2=1|F^{-1}\vec x|^2 = 1, that is x⃗T(FFT)−1x⃗=1\vec x^{\mathsf T}(FF^{\mathsf T})^{-1}\vec x = 1. The matrix B=FFTB = FF^{\mathsf T} is symmetric with positive eigenvalues λ1≥λ2\lambda_1 \ge \lambda_2 (v⃗TBv⃗=∣FTv⃗∣2>0\vec v^{\mathsf T}B\vec v = |F^{\mathsf T}\vec v|^2 > 0); in its perpendicular eigenvectors the equation reads x12/λ1+x22/λ2=1x_1^2/\lambda_1 + x_2^2/\lambda_2 = 1, an ellipse of semi-axes λ1\sqrt{\lambda_1} and λ2\sqrt{\lambda_2}. A line of material along the unit vector u⃗\vec u has the stretch ∣Fu⃗∣|F\vec u|, and ∣Fu⃗∣2=u⃗TFTFu⃗|F\vec u|^2 = \vec u^{\mathsf T}F^{\mathsf T}F\vec u lies between the eigenvalues of FTFF^{\mathsf T}F, which are those of FFTFF^{\mathsf T}. Finally λ1λ2=det⁡B=(det⁡F)2\lambda_1\lambda_2 = \det B = (\det F)^2. ∎

Definition 16.9 (Strain ellipse)

The strain ellipse is the ellipse into which a homogeneous strain turns a circle of radius 1; its semi-axes are the principal stretches S1≥S2S_1 \ge S_2, and its axes the principal directions of the strain.

Two strains that change the shape of a body equally can be very different.

Definition 16.10 (Pure shear, simple shear)

A pure shear is a homogeneous strain that keeps the area and keeps its principal directions fixed in the rock: F=(k001/k)F = \begin{pmatrix} k & 0 \\ 0 & 1/k\end{pmatrix} in those axes, with k>1k > 1. A simple shear moves every point parallel to one direction, the shear direction, by γ\gamma times its distance from a fixed plane parallel to it: F=(1γ01)F = \begin{pmatrix} 1 & \gamma \\ 0 & 1\end{pmatrix}.

Both keep the area, since both determinants are 1. In pure shear the lines of material along the axes of the strain ellipse are the same lines at every stage: the strain is coaxial. In simple shear they are not, as the next proposition and the figure after it show.

Proposition 16.11 (The ellipse of simple shear)

A simple shear γ\gamma has the principal stretches

S1,2=1+γ2/4±γ/2,S_{1,2} = \sqrt{1 + \gamma^2/4} \pm \gamma/2 ,

and the long axis of its strain ellipse makes with the shear direction the angle θ′\theta' given by tan⁡2θ′=2/γ\tan2\theta' = 2/\gamma.

Proof. FFT=(1+γ2γγ1)FF^{\mathsf T} = \begin{pmatrix} 1+\gamma^2 & \gamma \\ \gamma & 1\end{pmatrix} has the trace 2+γ22+\gamma^2 and the determinant 1. So S1S2=1S_1S_2 = 1 and S12+S22=2+γ2S_1^2 + S_2^2 = 2 + \gamma^2, hence (S1−S2)2=γ2(S_1 - S_2)^2 = \gamma^2, S1−S2=γS_1 - S_2 = \gamma, and S1=γ/2+1+γ2/4S_1 = \gamma/2 + \sqrt{1+\gamma^2/4}. The eigenvector of the largest eigenvalue of a symmetric matrix (abbd)\begin{pmatrix} a & b \\ b & d\end{pmatrix} makes with the first axis the angle given by tan⁡2θ′=2b/(a−d)\tan2\theta' = 2b/(a-d) (Theorem 16.3 is the same computation): here 2γ/γ2=2/γ2\gamma/\gamma^2 = 2/\gamma. ∎

A square of rock with its inscribed circle (a), deformed by a pure shear with k = 1.618 (b) and by a simple shear with = 1 (c), which has the same principal stretches, 1.618 and 0.618. Dashed blue: the axes of the strain ellipse; dashed grey: the square before. In pure shear the axes stay on the same lines of material; in simple shear the long axis lies at 31.7 to the shear direction, and the diagonal that was the direction of fastest stretching at the start (red) has already turned past it, to 26.6. The shapes are exact images of the square and the circle under the two matrices.
A square of rock with its inscribed circle (a), deformed by a pure shear with k=1.618k = 1.618 (b) and by a simple shear with γ=1\gamma = 1 (c), which has the same principal stretches, 1.618 and 0.618. Dashed blue: the axes of the strain ellipse; dashed grey: the square before. In pure shear the axes stay on the same lines of material; in simple shear the long axis lies at 31.7∘31.7{}^{\circ} to the shear direction, and the diagonal that was the direction of fastest stretching at the start (red) has already turned past it, to 26.6∘26.6{}^{\circ}. The shapes are exact images of the square and the circle under the two matrices.

The strain ellipse records the total, or finite, strain. A deformation that goes on for millions of years is the sum of many small increments, each an infinitesimal strain; for a small γ\gamma the proposition gives S1,2≈1±γ/2S_{1,2} \approx 1 \pm \gamma/2 and θ′≈45∘\theta' \approx 45{}^{\circ}. In simple shear the increments always stretch fastest at 45∘45{}^{\circ} to the shear direction, while the finite ellipse turns towards it, 31.7∘31.7{}^{\circ} at γ=1\gamma = 1, 22.5∘22.5{}^{\circ} at γ=2\gamma = 2, ever closer as γ\gamma grows. This is why flattened pebbles and stretched minerals in a zone of intense shear lie almost in its plane, and why the angle they make with the zone measures how far it has moved.

16.3 Rheology

Definition 16.12 (Rheology, brittle and ductile behaviour)

The rheology of a material is the way it deforms and flows under stress: the relation between stress, strain and the rate of strain. A rock shows brittle behaviour when it deforms by fracture or by sliding on fractures, on discrete surfaces, with a sudden loss of strength; it shows ductile behaviour when it deforms permanently and continuously through its volume, without losing its cohesion.

Rocks show all the behaviours of the physics books. Under small, brief stresses they are elastic: the strain is proportional to the stress, as in Hooke’s law, and disappears with it; seismic waves (Chapter 9) travel through elastic rock. Over long times the hot mantle flows like a very viscous fluid, the strain rate growing with the stress. In between, cold rock breaks and slides, and warm rock creeps. Which behaviour wins depends on the stress, the temperature, the pressure, the fluid in the pores and the time allowed.

Brittle failure

Definition 16.13 (Coulomb failure criterion)

A rock obeys the Coulomb failure criterion if a plane through it breaks, or an existing fracture slips, as soon as on that plane

τ=C+μ σn′,σn′=σn−P,\tau = C + \mu\,\sigma_n' , \qquad \sigma_n' = \sigma_n - P ,

where C≥0C \ge 0 is the cohesion of the rock, μ\mu its coefficient of internal friction and ϕ=arctan⁡μ\phi = \arctan\mu its angle of internal friction.

The criterion bears the names of Coulomb and Mohr. Its constants are measured on samples in the laboratory, and differ from rock to rock. An existing fracture has lost its cohesion: for it, C=0C = 0, and the friction on it hardly depends on the rock (Proposition 16.15), with μ\mu between 0.6 and 0.85, an angle of friction between 31∘31{}^{\circ} and 40∘40{}^{\circ}.

Theorem 16.14 (The angle of failure)

A rock obeying the Coulomb criterion first breaks on the planes that make the angle 45∘−ϕ/245{}^{\circ} - \phi/2 with the direction of σ1\sigma_1, on either side of it, and it breaks when

σ1′−σ3′2=Ccos⁡ϕ+σ1′+σ3′2 sin⁡ϕ.\frac{\sigma_1' - \sigma_3'}{2} = C\cos\phi + \frac{\sigma_1' + \sigma_3'}{2}\,\sin\phi .

Proof. Draw the Mohr circle in effective stresses, of centre c′=(σ1′+σ3′)/2c' = (\sigma_1'+\sigma_3')/2 and radius r=(σ1′−σ3′)/2r = (\sigma_1'-\sigma_3')/2 (figure below); the pore pressure has moved it by PP, since it takes PP from every normal stress and nothing from the shear. While the whole circle lies below the line τ=C+μσn′\tau = C + \mu\sigma_n', no plane breaks. As the stresses change, the first plane to break is the point where the circle touches the line. There the radius is perpendicular to the line; the line rises at the angle ϕ\phi above the horizontal, so the radius to the point of contact makes the angle 90∘+ϕ90{}^{\circ} + \phi with the direction of the σ1\sigma_1 end. By Proposition 16.5 this point is the plane whose normal makes the angle θ\theta with σ1\sigma_1, where 2θ=90∘+ϕ2\theta = 90{}^{\circ} + \phi; the plane itself makes 90∘−θ=45∘−ϕ/290{}^{\circ} - \theta = 45{}^{\circ} - \phi/2 with σ1\sigma_1, and the lower half of the circle gives the symmetric plane. Contact means that the distance from the centre to the line equals the radius: r=(C+μc′)/1+μ2=Ccos⁡ϕ+c′sin⁡ϕr = (C + \mu c')/\sqrt{1+\mu^2} = C\cos\phi + c'\sin\phi, since cos⁡ϕ=1/1+μ2\cos\phi = 1/\sqrt{1+\mu^2} and sin⁡ϕ=μ/1+μ2\sin\phi = \mu/\sqrt{1+\mu^2}. ∎

Mohr’s circle in effective stresses and a Coulomb envelope. A plane whose normal makes the angle  with _1 is the point at the angle 2 from the _1 end (orange). The circle drawn just touches the envelope: the plane at the point of contact breaks, its normal at = 45 + /2 from _1, the radius there perpendicular to the envelope. Drawn to scale for C = 10\, MPa, = 0.6 and _3' = 20\, MPa, which give _1' = 97.7\, MPa.
Mohr’s circle in effective stresses and a Coulomb envelope. A plane whose normal makes the angle θ\theta with σ1\sigma_1 is the point at the angle 2θ2\theta from the σ1\sigma_1 end (orange). The circle drawn just touches the envelope: the plane at the point of contact breaks, its normal at θ=45∘+ϕ/2\theta = 45{}^{\circ} + \phi/2 from σ1\sigma_1, the radius there perpendicular to the envelope. Drawn to scale for C=10 MPaC = 10\,\mathrm{MPa}, μ=0.6\mu = 0.6 and σ3′=20 MPa\sigma_3' = 20\,\mathrm{MPa}, which give σ1′=97.7 MPa\sigma_1' = 97.7\,\mathrm{MPa}.

With ϕ=30∘\phi = 30{}^{\circ}, a rock breaks on planes at 30∘30{}^{\circ} to σ1\sigma_1, and the two possible planes make 60∘60{}^{\circ} with each other, cut in two by σ1\sigma_1. This is the angle between the conjugate faults that are seen in the field, and the reason, as Chapter 17 shows, why normal faults dip steeply and thrusts gently.

For sliding on fractures that already exist, experiment gives the friction itself, and it gives it with a surprising simplicity.

Proposition 16.15 (Byerlee’s law)

For most rocks, sliding on an existing fracture or fault starts when the shear stress reaches

τ=0.85 σn′(σn′<200 MPa),τ=50 MPa+0.6 σn′(σn′>200 MPa),\tau = 0.85\,\sigma_n' \quad (\sigma_n' < 200\,\mathrm{MPa}), \qquad \tau = 50\,\mathrm{MPa} + 0.6\,\sigma_n' \quad (\sigma_n' > 200\,\mathrm{MPa}),

whatever the kind of rock: this is Byerlee’s law.

Proof. Admitted at this level. ∎

The law is a result of experiment, not of theory. James Byerlee measured, in 1975, the fracture strength and the frictional strength of a sandstone under confining and pore pressures, and found both governed by the effective stress alone, the difference between the two pressures; the strength of fracture varied by up to 20 %20\,\% with the cement between the grains, but the friction did not depend on the rock, and the same law held for gabbro, dunite, serpentinite, granite and limestone. The two lines meet at σn′=200 MPa\sigma_n' = 200\,\mathrm{MPa}, where both give 170 MPa170\,\mathrm{MPa}.

The law of effective stress is the key to the opening of this chapter. Raising the pore pressure by ΔP\Delta P lowers every effective normal stress by ΔP\Delta P and leaves every shear stress as it was: the Mohr circle slides to the left, unchanged in size, towards the failure line. A fault that was safe can be brought to slip without any change in the tectonic stress. The critical shear stress on a fault is τc=τ0+μ(σn−P)\tau_c = \tau_0 + \mu(\sigma_n - P), and injection works on its last term. At Denver the earthquakes kept to the rock where the pore pressure had risen by more than about 3.2 MPa3.2\,\mathrm{MPa}, as if that rise were what the faults there needed.

Method 16.16 (Testing a fault for slip)

To decide whether a fault at the depth zz will slip, and what would make it:

  1. Find the principal stresses in the plane perpendicular to the strike of the fault: σv=ρgz\sigma_v = \rho g z, and the horizontal stress, measured or assumed; take the pore pressure PP (hydrostatic, ρwgz\rho_w g z, if nothing else is known).
  2. Measure the angle θ\theta between the normal to the fault and the direction of σ1\sigma_1.
  3. Compute σn\sigma_n and τ\tau on the fault with Proposition 16.5, then σn′=σn−P\sigma_n' = \sigma_n - P.
  4. Compare τ\tau with the friction of Proposition 16.15: below it, the fault holds; τ/σn′\tau/\sigma_n' against 0.85 measures the margin.
  5. The rise of pore pressure that brings it to slip is ΔP=σn′−τ/0.85\Delta P = \sigma_n' - \tau/0.85 on the lower branch of the law (σn′−(τ−50)/0.6\sigma_n' - (\tau - 50)/0.6, in megapascals, on the upper one).

Ductile creep

Hot rock does not wait to break. Above a few hundred degrees in quartz-rich rock, and at higher temperatures in olivine, crystals deform by the slow movement of defects through their lattice, and the rock creeps at a rate that grows steeply with the stress and with the temperature.

Proposition 16.17 (Power-law creep)

At high temperature a rock deforming by dislocation creep flows at the strain rate

ε˙=A (σ1−σ3)nexp⁡(−E+PVRT),\dot\varepsilon = A\,(\sigma_1 - \sigma_3)^n \exp\Bigl(-\frac{E + PV}{RT}\Bigr),

where TT is the absolute temperature, PP the pressure, RR the gas constant, and AA, nn, EE (the activation energy) and VV (the activation volume) are constants of the material, measured in the laboratory. To flow at the rate ε˙\dot\varepsilon, it needs the differential stress

σ1−σ3=(ε˙A)1/nexp⁡(E+PVnRT).\sigma_1 - \sigma_3 = \Bigl(\frac{\dot\varepsilon}{A}\Bigr)^{1/n} \exp\Bigl(\frac{E + PV}{nRT}\Bigr).

Proof. Admitted at this level. ∎

The mechanisms behind the law are the subject of the Year 3 volume. Its constants come from experiments; for wet quartzite, n=4n = 4, E=223 kJ mol−1E = 223\,\mathrm{kJ}\,\mathrm{mol}^{-1} and A=1.1×10−4A = 1.1 \times 10^{-4} (stress in megapascals, time in seconds), after Gleason and Tullis (1995); for dry olivine, n=3.5n = 3.5, E=530 kJ mol−1E = 530\,\mathrm{kJ}\,\mathrm{mol}^{-1}, V=18 cm3 mol−1V = 18\,\mathrm{cm}^{3}\,\mathrm{mol}^{-1} and A=105A = 10^{5}, after Hirth and Kohlstedt (2003); R=8.314 462 618 J mol−1 K−1R = 8.314\,462\,618\,\mathrm{J}\,\mathrm{mol}^{-1}\,\mathrm{K}^{-1}.

Two features of the law shape the lithosphere. The stress depends only weakly on the rate: ten times faster asks only 101/4=1.7810^{1/4} = 1.78 times more stress of quartzite. And it depends enormously on the temperature: the exponential divides the strength of quartzite by several for each hundred degrees. Natural strain rates are slow. A belt of crust 300 km300\,\mathrm{km} wide that absorbs 1 cm1\,\mathrm{cm} of plate motion a year deforms at 0.01/(3.16×107×3×105)≈1×10−15 s−10.01/(3.16 \times 10^{7}\times3 \times 10^{5}) \approx 1 \times 10^{-15}\,\mathrm{s}^{-1}, the rate we shall use.

In the lab — Measuring the strength of rock

A high-pressure triaxial cell for measuring the strength of rock (Darryl Peroni, CSIRO, CC BY 3.0).

Rock-mechanics laboratories measure strength in a triaxial cell. A cylinder of rock, cored and ground flat at its ends, is sealed in a jacket of rubber or soft metal that keeps the confining fluid out of its pores. It sits in a thick-walled pressure vessel: oil around it sets the confining pressure, which plays the part of σ2=σ3\sigma_2 = \sigma_3; a piston bears on its ends and adds the axial load, σ1\sigma_1. A separate line fills the pores with water at a pressure of its own, so that the effective stress can be varied with the total stress fixed. The machine records the axial force and the shortening of the sample as it is loaded at a steady rate, until it breaks or, in a sample sawn across in advance, until the cut starts to slide. A furnace inside the vessel heats samples for experiments on creep, which are run at strain rates many orders of magnitude faster than any in the Earth and must be extrapolated to it.

16.4 The strength of the lithosphere

At every depth the lithosphere can fail in two ways: by sliding on faults, with a strength that grows with the effective pressure, or by creep, with a strength that falls as it gets hotter. It deforms in whichever way needs the smaller stress.

Definition 16.18 (Strength envelope, brittle–ductile transition, seismogenic layer)

The strength envelope of the lithosphere is the curve, against depth, of the largest differential stress it can bear at a given strain rate: at each depth, the smaller of the frictional strength and the creep strength. The brittle–ductile transition is the depth at which the two are equal: above it the rock deforms by faulting, below it by creep. The seismogenic layer is the range of depths in which most earthquakes start.

Proposition 16.19 (Frictional strength with depth)

In a layer of density ρ\rho with a hydrostatic pore pressure, one principal stress vertical, faults of every orientation and no cohesion, sliding with friction μ\mu starts at the differential stress

σ1−σ3=2μ1+μ2+μ ρgz(1−λ)if σv=σ1,σ1−σ3=2μ1+μ2−μ ρgz(1−λ)if σv=σ3,\begin{align*} \sigma_1 - \sigma_3 &= \frac{2\mu}{\sqrt{1+\mu^2} + \mu}\,\rho g z(1-\lambda) && \text{if $\sigma_v = \sigma_1$}, \\ \sigma_1 - \sigma_3 &= \frac{2\mu}{\sqrt{1+\mu^2} - \mu}\,\rho g z(1-\lambda) && \text{if $\sigma_v = \sigma_3$}, \end{align*}

with λ=ρw/ρ\lambda = \rho_w/\rho: the first case gives normal faults, the second thrusts.

Proof. The vertical effective stress is S=ρgz−ρwgz=ρgz(1−λ)S = \rho g z - \rho_w g z = \rho g z(1-\lambda). With C=0C = 0 and k=1+μ2k = \sqrt{1+\mu^2}, Theorem 16.14 says that a fault slips when r=μc′/kr = \mu c'/k, with rr the radius and c′c' the centre of the effective Mohr circle. If σv=σ1\sigma_v = \sigma_1, then σ1′=S\sigma_1' = S and c′=S−rc' = S - r, so rk=μS−μrrk = \mu S - \mu r and r=μS/(k+μ)r = \mu S/(k+\mu). If σv=σ3\sigma_v = \sigma_3, then c′=S+rc' = S + r and r=μS/(k−μ)r = \mu S/(k-\mu). The differential stress is 2r2r. ∎

With μ=0.85\mu = 0.85 and ρ=2700 kg m−3\rho = 2700\,\mathrm{kg}\,\mathrm{m}^{-3}, SS grows by 16.7 MPa16.7\,\mathrm{MPa} per kilometre and the frictional strength by 13.1 MPa13.1\,\mathrm{MPa} per kilometre under extension and 61.3 MPa61.3\,\mathrm{MPa} per kilometre under compression, nearly five times more: a crust is far easier to pull apart than to push together. Beyond an effective normal stress of 200 MPa200\,\mathrm{MPa} the upper branch of Byerlee’s law takes over, and the slope falls, in compression, to about 35 MPa35\,\mathrm{MPa} per kilometre.

Strength envelopes at the strain rate 10-15\, s-1. Red: frictional strength from Byerlee’s law with a hydrostatic pore pressure, for compression (thrust faulting, right) and extension (normal faulting, left, drawn as negative); blue: the creep strength of wet quartzite in the continental crust and of dry olivine in the mantle; black outline and shading: the strength, the smaller of the two at each depth. (a) A continent with a surface heat flow of 55\, mW\, m-2 and a crust 35\, km thick: strong upper crust, weak lower crust, strong uppermost mantle. (b) Ocean floor 60\, Myr old: a single strong layer, 38\, km thick in compression.
Strength envelopes at the strain rate 10−15 s−110^{-15}\,\mathrm{s}^{-1}. Red: frictional strength from Byerlee’s law with a hydrostatic pore pressure, for compression (thrust faulting, right) and extension (normal faulting, left, drawn as negative); blue: the creep strength of wet quartzite in the continental crust and of dry olivine in the mantle; black outline and shading: the strength, the smaller of the two at each depth. (a) A continent with a surface heat flow of 55 mW m−255\,\mathrm{mW}\,\mathrm{m}^{-2} and a crust 35 km35\,\mathrm{km} thick: strong upper crust, weak lower crust, strong uppermost mantle. (b) Ocean floor 60 Myr60\,\mathrm{Myr} old: a single strong layer, 38 km38\,\mathrm{km} thick in compression.

The figure above puts the two strengths together for two lithospheres. The continent has the geotherm of Chapter 10 with a surface heat flow of 55 mW m−255\,\mathrm{mW}\,\mathrm{m}^{-2}, a crust of wet quartzite 35 km35\,\mathrm{km} thick, and dry olivine below; the ocean floor is 60 Myr60\,\mathrm{Myr} old, with the half-space geotherm of the same chapter, and olivine from the sea floor down. The strain rate is 10−15 s−110^{-15}\,\mathrm{s}^{-1}. The 35 km35\,\mathrm{km} is the average depth of the Moho under the continents in the reference Earth model of Chapter 9.

Under the continent the brittle–ductile transition falls at 13.7 km13.7\,\mathrm{km} in compression, at 249∘C249{}^{\circ}\mathrm{C}, and at 17.1 km17.1\,\mathrm{km} in extension. A warmer crust would bring it up, a colder one push it down, since the creep law depends on the temperature alone at a given stress. The transition is the strongest level of the crust. Below it the strength collapses: at the Moho, at 527∘C527{}^{\circ}\mathrm{C}, quartzite flows under 7.6 MPa7.6\,\mathrm{MPa}, while olivine at the same temperature would need some 30 000 MPa30\,000\,\mathrm{MPa}, so far beyond the frictional strength that the top of the mantle is brittle again. A second transition follows at 44.6 km44.6\,\mathrm{km} in compression. The lower crust of this model is a soft layer between two strong ones: the “jelly sandwich”. Under the ocean the whole lithosphere is olivine, and the strength grows down to a single transition at 38.2 km38.2\,\mathrm{km}, at 641∘C641{}^{\circ}\mathrm{C}.

The earthquakes agree with the oceanic envelope: inside the oceanic plates, they reach depths where the temperature is 600 to 800∘C600\text{ to }800{}^{\circ}\mathrm{C}, close to the 641∘C641{}^{\circ}\mathrm{C} of the model’s single transition. Deeper earthquakes occur only where one plate sinks under another, down to more than 700 km700\,\mathrm{km} (Chapter 14).

The continental mantle is where the picture is disputed. For about twenty years the jelly sandwich was the prevailing view, built on laboratory measurements of dry olivine and on a few earthquakes thought to lie beneath the Moho. In 2002 James Jackson argued that it should be abandoned: better depths showed that earthquakes in the continents are confined to a single layer, usually the upper crust, sometimes the whole crust, with no convincing earthquakes in the mantle beneath, even where the Moho is only 300 to 500∘C300\text{ to }500{}^{\circ}\mathrm{C}. Small amounts of water, a few parts per million in olivine, are enough to weaken it dramatically, and the continental mantle may well hold that much; the strength of the continents would then lie mostly in their crust. The two views draw different envelopes from the same laws, with dry or wet olivine below the Moho.

Whichever is right, an envelope is a bound and not a measurement: the laboratory laws are extrapolated over many orders of magnitude of strain rate, and the peak stresses it shows, more than a gigapascal, are far above the 1 to 10 MPa1\text{ to }10\,\mathrm{MPa} that earthquakes are seen to release.

16.5 Exercises

Exercise 16.1 ★

Take a crust of density 2700 kg m−32700\,\mathrm{kg}\,\mathrm{m}^{-3} and g=9.81 m s−2g = 9.81\,\mathrm{m}\,\mathrm{s}^{-2}. At a depth of 10 km10\,\mathrm{km}, compute (a) the vertical stress, (b) the hydrostatic pore pressure, (c) the vertical effective stress and the pore-pressure ratio λ\lambda.

Solution

Solution of Exercise 16.1.

(a) σv=2700×9.81×10 000=2.65×108 Pa=264.9 MPa\sigma_v = 2700\times9.81\times10\,000 = 2.65 \times 10^{8}\,\mathrm{Pa} = 264.9\,\mathrm{MPa}. (b) P=1000×9.81×10 000=98.1 MPaP = 1000\times9.81\times10\,000 = 98.1\,\mathrm{MPa}. (c) σv′=264.9−98.1=166.8 MPa\sigma_v' = 264.9 - 98.1 = 166.8\,\mathrm{MPa}, and λ=98.1/264.9=0.370\lambda = 98.1/264.9 = 0.370, which is 1000/27001000/2700.

Exercise 16.2 ★

(a) A bed 10 km10\,\mathrm{km} long is stretched to 13 km13\,\mathrm{km}: give its extension and its stretch. (b) Another, 10 km10\,\mathrm{km} long, is shortened to 7 km7\,\mathrm{km}. (c) Two lines of a rock that were perpendicular now make an angle of 60∘60{}^{\circ}: what are the angular shear and the shear strain?

Solution

Solution of Exercise 16.2.

(a) e=(13−10)/10=0.30e = (13-10)/10 = 0.30 and S=1.30S = 1.30. (b) e=(7−10)/10=−0.30e = (7-10)/10 = -0.30, a shortening of 30 %30\,\%, and S=0.70S = 0.70. (c) The angle has closed by ψ=30∘\psi = 30{}^{\circ}, and γ=tan⁡30∘=0.577\gamma = \tan30{}^{\circ} = 0.577.

Exercise 16.3 ★

At a point, σ1=100 MPa\sigma_1 = 100\,\mathrm{MPa} and σ3=40 MPa\sigma_3 = 40\,\mathrm{MPa}. (a) Draw the Mohr circle. (b) What is the largest shear stress, on which planes does it act, and what normal stress acts on them? (c) Compute σn\sigma_n and τ\tau on the plane whose normal makes 30∘30{}^{\circ} with σ1\sigma_1.

Solution

Solution of Exercise 16.3.

(a) Centre 70 MPa70\,\mathrm{MPa}, radius 30 MPa30\,\mathrm{MPa}. (b) The largest shear stress is the radius, 30 MPa30\,\mathrm{MPa}, on the planes at 45∘45{}^{\circ} to σ1\sigma_1 and σ3\sigma_3, which carry the normal stress of the centre, 70 MPa70\,\mathrm{MPa}. (c) 2θ=60∘2\theta = 60{}^{\circ}: σn=70+30cos⁡60∘=85 MPa\sigma_n = 70 + 30\cos60{}^{\circ} = 85\,\mathrm{MPa} and τ=30sin⁡60∘=26.0 MPa\tau = 30\sin60{}^{\circ} = 26.0\,\mathrm{MPa}.

Exercise 16.4 ★

A rock has the cohesion 10 MPa10\,\mathrm{MPa} and the angle of internal friction 30∘30{}^{\circ}. (a) At what angle to σ1\sigma_1 does it break, and what angle do the two possible fracture planes make with each other? (b) With σ3′=20 MPa\sigma_3' = 20\,\mathrm{MPa}, what effective σ1′\sigma_1' breaks it?

Solution

Solution of Exercise 16.4.

(a) 45∘−30∘/2=30∘45{}^{\circ} - 30{}^{\circ}/2 = 30{}^{\circ} to σ1\sigma_1, on either side of it, so the two planes make 60∘60{}^{\circ} with each other. (b) With c′=20+rc' = 20 + r, the condition of Theorem 16.14 reads r=Ccos⁡ϕ+(20+r)sin⁡ϕr = C\cos\phi + (20 + r)\sin\phi, so

r=Ccos⁡ϕ+20sin⁡ϕ1−sin⁡ϕ=8.66+100.5=37.3 MPa,r = \frac{C\cos\phi + 20\sin\phi}{1 - \sin\phi} = \frac{8.66 + 10}{0.5} = 37.3\,\mathrm{MPa},

and σ1′=20+2r=94.6 MPa\sigma_1' = 20 + 2r = 94.6\,\mathrm{MPa}.

Exercise 16.5 ★★

In the axes xx (horizontal) and yy (vertical), σxx=60 MPa\sigma_{xx} = 60\,\mathrm{MPa}, σyy=20 MPa\sigma_{yy} = 20\,\mathrm{MPa} and σxy=15 MPa\sigma_{xy} = 15\,\mathrm{MPa}. (a) Compute the principal stresses and the angle θp\theta_p. (b) Check with Proposition 16.2 that the plane of normal θp\theta_p carries no shear stress and the normal stress σ1\sigma_1. (c) What is the largest shear stress at this point?

Solution

Solution of Exercise 16.5.

(a) c=40c = 40 and R=202+152=25 MPaR = \sqrt{20^2 + 15^2} = 25\,\mathrm{MPa}: σ1=65 MPa\sigma_1 = 65\,\mathrm{MPa} and σ3=15 MPa\sigma_3 = 15\,\mathrm{MPa}; tan⁡2θp=30/40=0.75\tan2\theta_p = 30/40 = 0.75, 2θp=36.87∘2\theta_p = 36.87{}^{\circ}, θp=18.43∘\theta_p = 18.43{}^{\circ}. (b) At this angle cos⁡2θ=0.9\cos^2\theta = 0.9, sin⁡2θ=0.1\sin^2\theta = 0.1 and sin⁡θcos⁡θ=0.3\sin\theta\cos\theta = 0.3: σn=60×0.9+2×15×0.3+20×0.1=54+9+2=65 MPa\sigma_n = 60\times0.9 + 2\times15\times0.3 + 20\times0.1 = 54 + 9 + 2 = 65\,\mathrm{MPa}, and τ=(20−60)×0.3+15×(0.9−0.1)=−12+12=0\tau = (20-60)\times0.3 + 15\times(0.9-0.1) = -12 + 12 = 0. (c) R=25 MPaR = 25\,\mathrm{MPa}, on the planes at 45∘45{}^{\circ} to the principal directions.

Exercise 16.6 ★★

A shear zone has deformed its rock by a simple shear γ=2\gamma = 2. (a) Compute the principal stretches and the angle of the long axis of the strain ellipse to the shear direction. (b) Check that the area has not changed. (c) A line of material was at 45∘45{}^{\circ} to the shear direction, rising in the sense of the shear: where does it lie now, and what is its stretch? Compare with (a).

Solution

Solution of Exercise 16.6.

(a) S1,2=1+1±1S_{1,2} = \sqrt{1 + 1} \pm 1: S1=2.414S_1 = 2.414 and S2=0.414S_2 = 0.414; tan⁡2θ′=2/2=1\tan2\theta' = 2/2 = 1, θ′=22.5∘\theta' = 22.5{}^{\circ}. (b) S1S2=(2+1)(2−1)=1S_1S_2 = (\sqrt2 + 1)(\sqrt2 - 1) = 1, which is det⁡F\det F: no change of area. (c) The line along (1,1)(1, 1) goes to F(1,1)=(1+2,1)=(3,1)F(1, 1) = (1 + 2, 1) = (3, 1), at arctan⁡(1/3)=18.4∘\arctan(1/3) = 18.4{}^{\circ} from the shear direction, with the stretch 10/2=2.24\sqrt{10}/\sqrt2 = 2.24. It has turned past the long axis of the ellipse, at 22.5∘22.5{}^{\circ}, towards the shear plane; its stretch is a little less than S1S_1, as it must be, since no line stretches more than S1S_1.

Exercise 16.7 ★★

In a shear zone 200 m200\,\mathrm{m} thick, small round spots in a slate have become ellipses with axes in the ratio 4 to 1. Assume a simple shear, with no change of area. (a) Find S1S_1, S2S_2 and γ\gamma. (b) At what angle to the walls of the zone should the long axes lie? (c) How far has one wall moved past the other?

Solution

Solution of Exercise 16.7.

(a) S1/S2=4S_1/S_2 = 4 and S1S2=1S_1S_2 = 1 give S1=2S_1 = 2 and S2=0.5S_2 = 0.5; by Proposition 16.11, γ=S1−S2=1.5\gamma = S_1 - S_2 = 1.5. (b) tan⁡2θ′=2/1.5=1.333\tan2\theta' = 2/1.5 = 1.333, 2θ′=53.1∘2\theta' = 53.1{}^{\circ}: the long axes should lie at 26.6∘26.6{}^{\circ} to the walls. (c) 1.5×200=300 m1.5\times200 = 300\,\mathrm{m}.

Exercise 16.8 ★★

A fault at a depth of 3 km3\,\mathrm{km}, in crust of density 2700 kg m−32700\,\mathrm{kg}\,\mathrm{m}^{-3}, carries the normal stress 70 MPa70\,\mathrm{MPa} and the shear stress 30 MPa30\,\mathrm{MPa}. (a) With a hydrostatic pore pressure, does it slip according to Byerlee’s law? (b) And if the pores are sealed and λ=0.6\lambda = 0.6? (c) Find the value of λ\lambda at which it starts to slip.

Solution

Solution of Exercise 16.8.

σv=2700×9.81×3000=79.46 MPa\sigma_v = 2700\times9.81\times3000 = 79.46\,\mathrm{MPa}. (a) P=29.43 MPaP = 29.43\,\mathrm{MPa}, σn′=70−29.43=40.57 MPa\sigma_n' = 70 - 29.43 = 40.57\,\mathrm{MPa}, and Byerlee allows 0.85×40.57=34.5 MPa0.85\times40.57 = 34.5\,\mathrm{MPa}, more than the 30 MPa30\,\mathrm{MPa} applied: the fault holds. (b) P=0.6×79.46=47.68 MPaP = 0.6\times79.46 = 47.68\,\mathrm{MPa}, σn′=22.32 MPa\sigma_n' = 22.32\,\mathrm{MPa}, and the friction gives only 19.0 MPa19.0\,\mathrm{MPa}: the fault slips. (c) 30=0.85 (70−79.46 λ)30 = 0.85\,(70 - 79.46\,\lambda) gives λ=(70−35.29)/79.46=0.437\lambda = (70 - 35.29)/79.46 = 0.437.

Exercise 16.9 ★★

Use the creep law of wet quartzite (Proposition 16.17). (a) By what factor must the stress rise to make it flow ten times faster? (b) By what factor does its strength fall between 400∘C400{}^{\circ}\mathrm{C} and 500∘C500{}^{\circ}\mathrm{C}, at the same rate and with V=0V = 0? (c) Explain with these two results why the depth of the brittle–ductile transition depends much more on the geotherm than on the strain rate.

Solution

Solution of Exercise 16.9.

(a) The stress goes as ε˙1/4\dot\varepsilon^{1/4}: 101/4=1.7810^{1/4} = 1.78. (b) The ratio of the strengths is

exp⁡[EnR(1673.15−1773.15)]=exp⁡(6705×1.921×10−4)=exp⁡(1.288)=3.63.\exp\Bigl[\frac{E}{nR}\Bigl(\frac{1}{673.15} - \frac{1}{773.15}\Bigr)\Bigr] = \exp\bigl(6705\times1.921 \times 10^{-4}\bigr) = \exp(1.288) = 3.63 .

(c) A tenfold change of rate changes the creep strength by a factor 1.78, which the temperature does in only 100×ln⁡1.78/ln⁡3.63≈45∘C100\times\ln1.78/\ln3.63 \approx 45{}^{\circ}\mathrm{C}; on a geotherm of about 20∘C20{}^{\circ}\mathrm{C} per kilometre, that moves the transition by about 2 km2\,\mathrm{km}. A change of geotherm moves the isotherms, and with them the transition, by far more.

Exercise 16.10 ★★★

Where the vertical stress is σ2\sigma_2, faults are strike-slip. Assume that the vertical effective stress is then the mean (σ1′+σ3′)/2(\sigma_1' + \sigma_3')/2. (a) Show that sliding with friction μ\mu and no cohesion starts at σ1−σ3=2μ ρgz(1−λ)/1+μ2\sigma_1 - \sigma_3 = 2\mu\,\rho g z(1-\lambda)/\sqrt{1+\mu^2}. (b) Compute the slope in megapascals per kilometre for μ=0.85\mu = 0.85 and ρ=2700 kg m−3\rho = 2700\,\mathrm{kg}\,\mathrm{m}^{-3}, and place it between the slopes of normal and thrust faulting. (c) Express each of the three slopes as a multiple of the vertical effective stress.

Solution

Solution of Exercise 16.10.

(a) With C=0C = 0, a fault slips when r=μc′/1+μ2r = \mu c'/\sqrt{1+\mu^2} (Theorem 16.14). Here c′=S=ρgz(1−λ)c' = S = \rho g z(1-\lambda), so σ1−σ3=2r=2μS/1+μ2\sigma_1 - \sigma_3 = 2r = 2\mu S/\sqrt{1+\mu^2}. (b) SS grows by 2700×9.81×1000×(1−1000/2700)=16.68 MPa2700\times9.81\times1000\times(1 - 1000/2700) = 16.68\,\mathrm{MPa} per kilometre, and 2×0.85/1.3124=1.2952\times0.85/1.3124 = 1.295: the slope is 21.6 MPa21.6\,\mathrm{MPa} per kilometre, between 13.113.1 (normal faults) and 61.3 MPa61.3\,\mathrm{MPa} per kilometre (thrusts). (c) 2μ/(k+μ)=0.7862\mu/(k+\mu) = 0.786, 2μ/k=1.2952\mu/k = 1.295 and 2μ/(k−μ)=3.682\mu/(k-\mu) = 3.68, with k=1.3124k = 1.3124: the differential stress at slip is 0.79, 1.30 and 3.68 times the vertical effective stress.

Exercise 16.11 ★★★

Model the oceanic lithosphere 60 Myr60\,\mathrm{Myr} old as a half-space cooled from 1350∘C1350{}^{\circ}\mathrm{C}, with a surface at 0∘C0{}^{\circ}\mathrm{C} and κ=10−6 m2 s−1\kappa = 10^{-6}\,\mathrm{m}^{2}\,\mathrm{s}^{-1}: T=1350erf⁡(z/(2κt))T = 1350\operatorname{erf}\bigl(z/(2\sqrt{\kappa t})\bigr). (a) Compute 2κt2\sqrt{\kappa t}. (b) Find the depths of the 600∘C600{}^{\circ}\mathrm{C} and 800∘C800{}^{\circ}\mathrm{C} isotherms. (c) Earthquakes inside the oceanic plates reach the depths where the temperature is 600 to 800∘C600\text{ to }800{}^{\circ}\mathrm{C}. Compare with the brittle–ductile transition in the oceanic strength envelope of this chapter, at 38.2 km38.2\,\mathrm{km} and 641∘C641{}^{\circ}\mathrm{C}.

Solution

Solution of Exercise 16.11.

(a) t=60×106×3.156×107=1.89×1015 st = 60\times10^{6}\times3.156 \times 10^{7} = 1.89 \times 10^{15}\,\mathrm{s} and 2κt=21.89×109=87.0 km2\sqrt{\kappa t} = 2\sqrt{1.89 \times 10^{9}} = 87.0\,\mathrm{km}. (b) erf⁡x=600/1350=0.444\operatorname{erf}x = 600/1350 = 0.444 for x=0.417x = 0.417: z=0.417×87.0=36.3 kmz = 0.417\times87.0 = 36.3\,\mathrm{km}; erf⁡x=800/1350=0.593\operatorname{erf}x = 800/1350 = 0.593 for x=0.586x = 0.586: z=51.0 kmz = 51.0\,\mathrm{km}. (c) The earthquakes should reach 36 to 51 km36\text{ to }51\,\mathrm{km}; the envelope puts the base of the brittle layer at 38.2 km38.2\,\mathrm{km}, within that range and near its top, at a temperature, 641∘C641{}^{\circ}\mathrm{C}, in the range observed.

Exercise 16.12 ★★★

A rock is crossed by fractures of every orientation, all containing the direction of σ2\sigma_2, with no cohesion and friction 0.85. The effective principal stresses are σ1′=110 MPa\sigma_1' = 110\,\mathrm{MPa} and σ3′=20 MPa\sigma_3' = 20\,\mathrm{MPa}. (a) Show that some fractures slip. (b) Find the range of the angle between the slipping fractures and σ1\sigma_1. Which one is in the middle of the range? (c) Down to what value of σ1′\sigma_1', with σ3′\sigma_3' fixed, does at least one fracture still slip?

Solution

Solution of Exercise 16.12.

(a) r=45r = 45 and c′=65 MPac' = 65\,\mathrm{MPa}; the distance from the centre to the line τ=0.85σn′\tau = 0.85\sigma_n' is 0.85×65/1.3124=42.1 MPa0.85\times65/1.3124 = 42.1\,\mathrm{MPa}, less than the radius: the circle crosses the line, and the planes on the arc above it slip. (b) With 2θ2\theta the angle from the σ1\sigma_1 end, slip needs 45sin⁡2θ≥0.85 (65+45cos⁡2θ)45\sin2\theta \ge 0.85\,(65 + 45\cos2\theta), that is 45sin⁡2θ−38.25cos⁡2θ≥55.2545\sin2\theta - 38.25\cos2\theta \ge 55.25, or 59.06sin⁡(2θ−40.36∘)≥55.2559.06\sin(2\theta - 40.36{}^{\circ}) \ge 55.25, where 40.36∘=ϕ40.36{}^{\circ} = \phi. So sin⁡(2θ−ϕ)≥0.9355\sin(2\theta - \phi) \ge 0.9355, 2θ−ϕ2\theta - \phi between 69.31∘69.31{}^{\circ} and 110.69∘110.69{}^{\circ}, 2θ2\theta between 109.67∘109.67{}^{\circ} and 151.06∘151.06{}^{\circ}: the normals lie at 54.8∘54.8{}^{\circ} to 75.5∘75.5{}^{\circ} from σ1\sigma_1, and the slipping fractures at 14.5∘14.5{}^{\circ} to 35.2∘35.2{}^{\circ} from σ1\sigma_1. The middle of the range, 24.8∘24.8{}^{\circ}, is 45∘−ϕ/245{}^{\circ} - \phi/2, the plane of Theorem 16.14. (c) Only that plane slips when the circle just touches the line: r=μ(20+r)/kr = \mu(20 + r)/k, r=20μ/(k−μ)=17/0.4624=36.8 MPar = 20\mu/(k - \mu) = 17/0.4624 = 36.8\,\mathrm{MPa}, and σ1′=20+2r=93.5 MPa\sigma_1' = 20 + 2r = 93.5\,\mathrm{MPa}.

16.6 Problem: Will the fault slip?

Problem 16.1

Weekend problem — the stress on a normal fault at a depth of five kilometres, its safety margin, and the rise of pore pressure that would make it slip

A fault strikes north–south and dips 60∘60{}^{\circ} to the east. A disposal well reaches it at a depth of 5.00 km5.00\,\mathrm{km}, in crust of density 2700 kg m−32700\,\mathrm{kg}\,\mathrm{m}^{-3} whose pores connect to the surface. A measurement in the well gives the horizontal stress perpendicular to the fault, 75.0 MPa75.0\,\mathrm{MPa}; the horizontal stress along the strike lies between it and the vertical stress, so the problem is two-dimensional in the vertical plane east–west. Take g=9.81 m s−2g = 9.81\,\mathrm{m}\,\mathrm{s}^{-2}, water of density 1000 kg m−31000\,\mathrm{kg}\,\mathrm{m}^{-3} and Byerlee’s law. Give stresses to 0.01 MPa0.01\,\mathrm{MPa}.

Part I — The state of stress.

  1. Compute the vertical stress at the depth of the fault.
  2. Compute the hydrostatic pore pressure there, and the ratio λ\lambda.
  3. Which of the two stresses is σ1\sigma_1 and which σ3\sigma_3? What kind of fault does this state of stress drive?
  4. Compute the differential stress, the centre and the radius of the Mohr circle.
  5. Compute the effective principal stresses and the centre of the effective circle.
  6. With xx horizontal to the east and yy vertical, write the three components σxx\sigma_{xx}, σyy\sigma_{yy}, σxy\sigma_{xy}. Why is σxy\sigma_{xy} zero?

Part II — The stresses on the fault.

  1. Give the unit normal to the fault in the axes of question 6, and the angle θ\theta between it and σ1\sigma_1.
  2. Compute σn\sigma_n and τ\tau on the fault with Proposition 16.2.
  3. Check both values with Mohr’s circle: at what angle from the σ1\sigma_1 end does the fault lie?
  4. Compute the effective normal stress on the fault.
  5. Compute the ratio τ/σn′\tau/\sigma_n' and compare it with 0.85.
  6. What shear stress would make the fault slip under the present effective normal stress? By how many megapascals is it short?

Part III — Mohr’s circle and Byerlee’s law.

  1. Draw the effective Mohr circle and Byerlee’s line to scale.
  2. Compute the distance from the centre of the circle to the line and compare it with the radius. Can any plane through the rock slip?
  3. Which plane would slip first? Give its angle to σ1\sigma_1 and its dip.
  4. With Proposition 16.19, compute the differential stress at which normal faults slip at this depth, and check it against the slope of 13.1 MPa13.1\,\mathrm{MPa} per kilometre.
  5. How low would the horizontal stress have to fall for the best-oriented plane to slip?
  6. How low for the fault of the problem to slip? Explain why it is lower.

Part IV — Injection.

  1. Explain why a rise ΔP\Delta P of the pore pressure moves the effective circle by ΔP\Delta P to the left without changing its radius.
  2. Compute the rise of pore pressure that brings the best-oriented plane to slip.
  3. The well is full of water. What extra pressure must the pump apply at the wellhead to raise the pore pressure at the fault by that amount? How high a column of water is it equivalent to?
  4. If the friction on the fault were 0.6 rather than 0.85, would it be slipping already? What does the quiet of the fault say about its friction?
  5. At what ratio λ\lambda does the best-oriented plane slip?
  6. To one decimal, in megapascals, what rise of pore pressure brings this fault to slip?
Solution

Solution of Problem 16.1.

1. σv=2700×9.81×5000=132.44 MPa\sigma_v = 2700\times9.81\times5000 = 132.44\,\mathrm{MPa}.

2. P=1000×9.81×5000=49.05 MPaP = 1000\times9.81\times5000 = 49.05\,\mathrm{MPa}, and λ=49.05/132.44=0.370\lambda = 49.05/132.44 = 0.370.

3. σ1=σv=132.44 MPa\sigma_1 = \sigma_v = 132.44\,\mathrm{MPa}, vertical, and σ3=75.00 MPa\sigma_3 = 75.00\,\mathrm{MPa}, horizontal east–west: the crust is being stretched east–west under its own weight, the state that drives normal faults, such as this one.

4. σ1−σ3=57.44 MPa\sigma_1 - \sigma_3 = 57.44\,\mathrm{MPa}; centre (132.44+75.00)/2=103.72 MPa(132.44 + 75.00)/2 = 103.72\,\mathrm{MPa}; radius 28.72 MPa28.72\,\mathrm{MPa}.

5. σ1′=132.44−49.05=83.39 MPa\sigma_1' = 132.44 - 49.05 = 83.39\,\mathrm{MPa}, σ3′=75.00−49.05=25.95 MPa\sigma_3' = 75.00 - 49.05 = 25.95\,\mathrm{MPa}, centre 103.72−49.05=54.67 MPa103.72 - 49.05 = 54.67\,\mathrm{MPa}.

6. σxx=75.00 MPa\sigma_{xx} = 75.00\,\mathrm{MPa}, σyy=132.44 MPa\sigma_{yy} = 132.44\,\mathrm{MPa} and σxy=0\sigma_{xy} = 0: the axes are the principal directions, one of them vertical, so the planes perpendicular to them carry no shear stress.

7. Down its dip the fault runs along the unit vector (cos⁡60∘,−sin⁡60∘)(\cos60{}^{\circ}, -\sin60{}^{\circ}), east and down; its upward normal is n⃗=(sin⁡60∘,cos⁡60∘)=(0.866,0.500)\vec n = (\sin60{}^{\circ}, \cos60{}^{\circ}) = (0.866, 0.500), at 30∘30{}^{\circ} from xx. Its angle with σ1\sigma_1, along yy, has the cosine 0.500: θ=60∘\theta = 60{}^{\circ}.

8. With 30∘30{}^{\circ} from xx: σn=75.00×0.75+132.44×0.25=56.25+33.11=89.36 MPa\sigma_n = 75.00\times0.75 + 132.44\times0.25 = 56.25 + 33.11 = 89.36\,\mathrm{MPa}, and τ=(132.44−75.00)×sin⁡30∘cos⁡30∘=57.44×0.4330=24.87 MPa\tau = (132.44 - 75.00)\times \sin30{}^{\circ}\cos30{}^{\circ} = 57.44\times0.4330 = 24.87\,\mathrm{MPa}.

9. At 2θ=120∘2\theta = 120{}^{\circ} from the σ1\sigma_1 end: σn=103.72+28.72cos⁡120∘=103.72−14.36=89.36 MPa\sigma_n = 103.72 + 28.72\cos120{}^{\circ} = 103.72 - 14.36 = 89.36\,\mathrm{MPa} and τ=28.72sin⁡120∘=24.87 MPa\tau = 28.72\sin120{}^{\circ} = 24.87\,\mathrm{MPa}.

10. σn′=89.36−49.05=40.31 MPa\sigma_n' = 89.36 - 49.05 = 40.31\,\mathrm{MPa}.

11. 24.87/40.31=0.61724.87/40.31 = 0.617, below 0.85: the fault holds.

12. 0.85×40.31=34.26 MPa0.85\times40.31 = 34.26\,\mathrm{MPa}; the shear stress falls short of it by 9.39 MPa9.39\,\mathrm{MPa}.

13. The circle has its centre at 54.67 MPa54.67\,\mathrm{MPa} and the radius 28.72 MPa28.72\,\mathrm{MPa}, from 25.9525.95 to 83.39 MPa83.39\,\mathrm{MPa}; Byerlee’s line is τ=0.85 σn′\tau = 0.85\,\sigma_n' (all normal stresses here are below 200 MPa200\,\mathrm{MPa}); the fault is the point (40.31,24.87)(40.31, 24.87), at 120∘120{}^{\circ} from the σ1\sigma_1 end.

14. 0.85×54.67/1+0.852=46.47/1.3124=35.41 MPa0.85\times54.67/\sqrt{1 + 0.85^2} = 46.47/1.3124 = 35.41\,\mathrm{MPa}, more than the radius, 28.72 MPa28.72\,\mathrm{MPa}: the whole circle lies below the line, and no plane through the rock can slip.

15. ϕ=arctan⁡0.85=40.36∘\phi = \arctan0.85 = 40.36{}^{\circ}: the plane at 45∘−ϕ/2=24.8∘45{}^{\circ} - \phi/2 = 24.8{}^{\circ} from the vertical σ1\sigma_1, dipping 65.2∘65.2{}^{\circ}.

16. S=σv′=83.39 MPaS = \sigma_v' = 83.39\,\mathrm{MPa} and σ1−σ3=2×0.85×83.39/(1.3124+0.85)=65.55 MPa\sigma_1 - \sigma_3 = 2\times0.85\times83.39/(1.3124 + 0.85) = 65.55\,\mathrm{MPa}; the slope gives 13.11×5=65.55 MPa13.11\times5 = 65.55\,\mathrm{MPa}.

17. σ3=132.44−65.55=66.88 MPa\sigma_3 = 132.44 - 65.55 = 66.88\,\mathrm{MPa}.

18. The fault slips when rsin⁡120∘=0.85 (c′+rcos⁡120∘)r\sin120{}^{\circ} = 0.85\,(c' + r\cos120{}^{\circ}) with c′=(83.39+σ3′)/2c' = (83.39 + \sigma_3')/2 and r=(83.39−σ3′)/2r = (83.39 - \sigma_3')/2; solving gives σ3′=17.18 MPa\sigma_3' = 17.18\,\mathrm{MPa}, σ3=66.23 MPa\sigma_3 = 66.23\,\mathrm{MPa}. It is lower than for the best plane: the fault does not lie at the point where the circle first touches the line, so the circle must grow further before it reaches the fault’s own point.

19. Every effective normal stress, σ1′\sigma_1' and σ3′\sigma_3' included, falls by ΔP\Delta P, and their difference does not change; the shear stresses do not depend on the pore pressure at all.

20. The best plane slips when the distance equals the radius: 0.85 (54.67−ΔP)/1.3124=28.720.85\,(54.67 - \Delta P)/1.3124 = 28.72, so ΔP=54.67−28.72×1.3124/0.85=54.67−44.34=10.33 MPa\Delta P = 54.67 - 28.72\times1.3124/0.85 = 54.67 - 44.34 = 10.33\,\mathrm{MPa}.

21. The column of water in the well weighs the same as before, so the pump must add the whole 10.33 MPa10.33\,\mathrm{MPa} at the wellhead, about 103 times the atmospheric pressure: the weight of a column of water 10.33×106/(1000×9.81)=1053 m10.33 \times 10^{6}/(1000\times9.81) = 1053\,\mathrm{m} high.

22. With μ=0.6\mu = 0.6 the fault could bear only 0.6×40.31=24.19 MPa0.6\times40.31 = 24.19\,\mathrm{MPa}, less than the 24.87 MPa24.87\,\mathrm{MPa} it carries: it would be slipping already. Since it is quiet, its friction is at least 0.6170.617, or it has some cohesion.

23. The best-oriented plane slips when the pore pressure reaches 49.05+10.33=59.38 MPa49.05 + 10.33 = 59.38\,\mathrm{MPa}, that is λ=59.38/132.44=0.448\lambda = 59.38/132.44 = 0.448, well short of the lithostatic value 1.

24. ΔP=σn′−τ/0.85=40.309−24.870/0.85=40.309−29.259=11.049 MPa\Delta P = \sigma_n' - \tau/0.85 = 40.309 - 24.870/0.85 = 40.309 - 29.259 = 11.049\,\mathrm{MPa}, more than the 10.33 MPa10.33\,\mathrm{MPa} that would move a plane of the best orientation. To one decimal, the rise of pore pressure that brings the fault to slip is 11.0 MPa11.0\,\mathrm{MPa}.

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