This benchmark explores a 2D plane strain granite disk subjected to thermal loading. The outer radius is \( R_{\text{out}} = 1 \,\text{m} \), and the inner heated core has a radius of \( R_{\text{in}} = 0.2 \,\text{m} \).
🔧 Basic Setup:
• The core region has a higher thermal expansion coefficient:
\( \alpha_{t,\text{core}} = 4.3 \times 10^{-5} \,\text{m/m-°C} \), compared to the outer region:
\( \alpha_{t,\text{outer}} = 3.5 \times 10^{-5} \,\text{m/m-°C} \).
• The temperature in the core is increased from 25 °C to 100 °C.
🔬 Four simulation cases:
1. Case 1: Crack propagation in the core is prevented by setting \( d = 0 \).
2. Case 2: Crack is allowed everywhere, but \( G_{c,\text{core}} = 3.0 \times 10^{-3} \,\text{MPa·m} \),
\( G_{c,\text{outer}} = 3.0 \times 10^{-5} \,\text{MPa·m} \).
3. Case 3: Crack is allowed everywhere, and fracture toughness is uniform:
\( G_{c,\text{core}} = G_{c,\text{outer}} = 3.0 \times 10^{-5} \,\text{MPa·m} \).
4. Case 4: Same as Case 2, but core temperature only rises from 25 °C to 50 °C.
The model solves three governing equations: phase field fracture (PF), mechanical equilibrium, and heat conduction equation. Their interactions are summarized as:
🔁 Equilibrium ↔ Heat Conduction Equation:
• \( \mathbf{u} \) contributes to total strain \( \epsilon = \nabla^{\text{sym}}\mathbf{u} \).
• Temperature \( \theta \) is used to compute the trial undamaged stress \( \sigma_0 \), which is passed into the phase-field model.
🔁 Heat Conduction Equation ↔ Phase Field:
• The damage variable \( d \) affects thermal conductivity \( k \), which is assumed to drop to 2% of the intact value when fully damaged.
• In some models, the energy release rate \( G_c \) depends on \( d \) or \( \theta \), but that’s typically for high-temperature scenarios — not considered here.
🔁 Equilibrium ↔ Phase Field:
• \( \mathbf{u} \) feeds into phase-field through the elastic energy \( \Psi_{\text{elastic}} \) and an additional driving force term \( c_e \).
• The damage field \( d \) then degrades \( \sigma_0 \) to compute the final stress \( \sigma \).
✅ Implementation of coupling system by loosely coupled setting.
✅ Manually established interaction between thermal and phase field systems.
⚠️ Note 1: Any physical system is associated with a corresponding energy contribution, which can enter the phase-field fracture governing equation as part of the local driving force term. This is often written as: \[ \frac{\partial \Psi_{\text{loc}}}{\partial d} = \frac{\partial \Psi_{\text{elastic}}}{\partial d} + \frac{\partial \Psi_{\text{fracture}}}{\partial d} + \frac{\partial \Psi_{\text{other}}}{\partial d} \] where \(\Psi_{\text{other}}\) may represent additional physics such as thermal energy (\(\Psi_{\text{thermal}}\)) or fluid energy (\(\Psi_{\text{fluid}}\)) in porous flow systems. However, in a physical sense, thermally induced fracture arises primarily from the thermal stress, not from the temperature itself. As a result, it is common practice to exclude \(\Psi_{\text{thermal}}\) from the governing phase-field equation. Instead, temperature-dependent material parameters (e.g., conductivity in the present case) are coupled with the damage variable \(d\), capturing the thermal effects indirectly but effectively.
⚠️ Note 2: While using loosely coupled systems may compromise accuracy, extra care on convergence criteria is required. In this case, the nonlinear residual tolerance is set to \( 1 \times 10^{-7} \).
⚠️ Note 3: Theoretically, since thermal conductivity \( k \) becomes a spatially varying variable due to its coupling with damage \( d \),
the heat conduction equation should be modified from:
\[
\rho c \dot{\theta} - \rho r - k \nabla^2 \theta = 0
\]
to:
\[
\rho c \dot{\theta} - \rho r - k \nabla^2 \theta - \nabla k \cdot \nabla \theta = 0
\]
However, MOOSE does not natively support spatial derivatives of material properties in the heat kernel.
Therefore, for simplicity, the additional term \( \nabla k \cdot \nabla \theta \) is neglected in this benchmark.
One possible workaround is to convert the spatially varying material into an auxiliary variable and then manually define its gradients across each dimension.
This strategy is applied in the fatigue benchmark (Benchmark 5), but for a similar term in the phase field equation instead.
Case 1: Core Fixed
Case 2: Weak Outer Shell
Case 3: Uniform Toughness
Case 4: Lower Heating
✅ From Case 1 and Case 2, the fracture patterns differ due to whether damage in the core is allowed or not.
✅ In Case 3, since both core and outer shell share the same toughness, and the core is laterally confined, damage spreads more uniformly. This is likely influenced by the adopted phase-field formulation without elastic energy decomposition — hence compressive stress may also trigger damage. Here, tensile and compressive contributions are differentiated using the finite-epsilon model.
✅ In Case 4, the crack propagation is less aggressive than in Case 2, which aligns with expectations due to the lower temperature rise.