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Sequential Methods for Coupled Geomechanics and Multiphase Flow

Sequential Methods for Coupled Geomechanics and Multiphase Flow

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5.6. NUMERICAL EXAMPLES 143<br />

coupling strength is less than one (τ = 0.95, Fig. 5.4 (top)). The stability of the fixed-strain<br />

split is not improved by reducing the time step size. Thus, physical problems with large<br />

coupling strength (τ > 1) cannot be solved by the fixed-strain split (Fig. 5.4 (bottom)).<br />

The results from Figures 5.2–5.4 indicate that the stability criterion of the fixed-strain<br />

split is quite sharp. The fixed-strain split yields severe oscillatory behaviors even in its<br />

stability range, which is explained by the negative amplification factor.<br />

Midpoint rule <strong>for</strong> time integration<br />

We consider the midpoint rule <strong>for</strong> time discretization (α = 0.5 <strong>for</strong> both mechanics <strong>and</strong><br />

flow). Here, Kdr = 1 GPa <strong>and</strong> the other data are the same as Case 5.2. Figure 5.5 shows<br />

the stability behaviors <strong>for</strong> α = 0.5 when τ = 0.83 (top) <strong>and</strong> τ = 1.11 (bottom). The<br />

fixed-strain split is stable when τ < 1 whereas it is unstable when τ > 1, which supports<br />

our a-priori stability estimates from the Von Neumann method. Furthermore, while the<br />

drained split with the midpoint rule is unconditionally unstable, as shown in Chapter 3,<br />

the fixed-strain split with the midpoint rule is conditionally stable. The fixed-stress split,<br />

however, is unconditionally stable when τ ≥ 1, as shown in the bottom plot of Figure 5.5.<br />

This supports the a-priori stability estimate in Equations 5.17 <strong>and</strong> 5.24.<br />

The deviation factor η<br />

We use Case 5.2 with the backward Euler time discretization in order to validate the stability<br />

estimate of Equation 5.26, where τ = 3.33 <strong>and</strong> τ = ∞. From Equation 5.26, the stability<br />

condition becomes η ≥ 0.35 <strong>for</strong> τ = 3.33 <strong>and</strong> η ≥ 0.5 <strong>for</strong> τ = ∞. Figure 5.6 shows the<br />

pressure history with respect to time <strong>for</strong> τ = 3.33 <strong>and</strong> τ = ∞. On the top of Figure 5.6, η =<br />

0.33 leads to instability, but η = 0.37 yields a stable solution when τ = 3.33. The bottom<br />

of Figure 5.6 also shows that η = 0.48 causes instability whereas η = 0.52 leads to stability<br />

when τ = ∞. Figure 5.6 supports the fact that the stability estimate of Equation 5.26 is<br />

quite sharp.

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