# The 2D cylindrical shell benchmarks by Davies et al.#

*This section was contributed by William Durkin and Wolfgang Bangerth.*

All of the benchmarks presented so far take place in a Cartesian domain. Davies et al. describe a benchmark (in a paper that is currently still being written) for a 2D spherical Earth that is nondimensionalized such that

\(r_{\min}\) = 1.22 |
\( T |_{r_{min}} = 1\) |

\(r_{\max}\) = 2.22 |
\( T |_{r_{max}} = 0\) |

The benchmark is run for a series of approximations (Boussinesq, Extended Boussinesq, Truncated Anelastic Liquid, and Anelastic Liquid), and temperature, velocity, and heat flux calculations are compared with the results of other mantle modeling programs. will output all of these values directly except for the Nusselt number, which we must calculate ourselves from the heat fluxes that can compute. The Nusselt number of the top and bottom surfaces, \({Nu}_T\) and \({Nu}_B\), respectively, are defined by the authors of the benchmarks as

and

where \(f\) is the ratio \(\frac{r_{\min}}{r_{\max}}\).

We can put this in terms of heat flux

through the inner and outer surfaces, where \(q_r\) is heat flux in the radial direction. Let \(Q\) be the total heat that flows through a surface,

then (44) becomes

and similarly

\(Q_T\) and \(Q_B\) are
heat fluxes that can readily compute through the `heat flux statistics`

postprocessor (see Parameter name: List of postprocessors). For
further details on the nondimensionalization and equations used for each
approximation, refer to Davies et al.

The series of benchmarks is then defined by a number of cases relating to the exact equations chosen to model the fluid. We will discuss these in the following.

## Case 1.1: BA_Ra104_Iso_ZS.#

This case is run with the following settings:

Boussinesq Approximation

Boundary Condition: Zero-Slip

Rayleigh Number = \(10^4\)

Initial Conditions: \(D = 0, O = 4\)

\(\eta(T) = 1\)

where \(D\) and \(O\) refer to the degree and order of a spherical harmonic that describes the initial temperature. While the initial conditions matter, what is important here though is that the system evolve to four convective cells since we are only interested in the long term, steady state behavior.

The model is relatively straightforward to set up, basing the input file on that discussed in Section Simple convection in a quarter of a 2d annulus. The full input file can be found at benchmarks/davies_et_al/case-1.1.prm, with the interesting parts excerpted as follows:

```
############### Parameters describing the model
subsection Geometry model
set Model name = spherical shell
subsection Spherical shell
set Inner radius = 1.22
set Opening angle = 360
set Outer radius = 2.22
end
end
# [...]
subsection Material model
set Model name = simple
subsection Simple model
set Reference density = 1
set Reference specific heat = 1.
set Reference temperature = 0
set Thermal conductivity = 1
set Thermal expansion coefficient = 1e-6
set Viscosity = 1
end
end
############### Parameters describing the temperature field
# Angular mode is set to 4 in order to match the number of
# convective cells reported by Davies et al.
subsection Initial temperature model
set Model name = spherical hexagonal perturbation
subsection Spherical hexagonal perturbation
set Angular mode = 4
set Rotation offset = 0
end
end
############### Prescribe the Rayleigh number as g*alpha
# Here, Ra = 10^4 and alpha was chosen as 10^-6 above.
subsection Gravity model
set Model name = radial constant
subsection Radial constant
set Magnitude = 1e10
end
end
# [...]
```

We use the same trick here as in Convection in a 2d box to produce a model in which the density \(\rho(T)\) in the temperature equation (3) is almost constant (namely, by choosing a very small thermal expansion coefficient) as required by the benchmark, and instead prescribe the desired Rayleigh number by choosing a correspondingly large gravity.

Results for this and the other cases are shown below.

## Case 2.1: BA_Ra104_Iso_FS.#

Case 2.1 uses the following setup, differing only in the boundary conditions:

Boussinesq Approximation

Boundary Condition: Free-Slip

Rayleigh Number = \(10^4\)

Initial Conditions: \(D = 0, O = 4\)

\(\eta(T) = 1\)

As a consequence of the free slip boundary conditions, any solid body rotation of the entire system satisfies the Stokes equations with their boundary conditions. In other words, the solution of the problem is not unique: given a solution, adding a solid body rotation yields another solution. We select arbitrarily the one that has no net rotation (see Nullspace removal). The section in the input file that is relevant is then as follows (the full input file resides at benchmarks/davies_et_al/case-2.1.prm):

```
subsection Nullspace removal
set Remove nullspace = net rotation
end
subsection Boundary temperature model
set Fixed temperature boundary indicators = 0,1
end
subsection Boundary velocity model
set Tangential velocity boundary indicators = 0,1
end
```

Again, results are shown below.

## Case 2.2: BA_Ra105_Iso_FS.#

Case 2.2 is described as follows:

Boussinesq Approximation

Boundary Condition: Free-Slip

Rayleigh Number = \(10^5\)

Initial Conditions: Final conditions of case 2.1 (BA_Ra104_Iso_FS)

\(\eta(T) = 1\)

In other words, we have an increased Rayleigh number and begin with the final steady state of case 2.1. To start the model where case 2.1 left off, the input file of case 2.1, benchmarks/davies_et_al/case-2.1.prm, instructs to checkpoint itself every few time steps (see Checkpoint/restart support). If case 2.2 uses the same output directory, we can then resume the computations from this checkpoint with an input file that prescribes a different Rayleigh number and a later input time:

```
############### Global parameters
# Case 2.2 begins with the final steady state solution of Case 2.1
# "Resume computation" must be set to true, and "Output directory" must
# point to the folder that contains the results of Case 2.1.
set CFL number = 10
set End time = 3
set Output directory = output
set Resume computation = true
```

We increase the Rayleigh number to \(10^5\) by increasing the magnitude of gravity in the input file. The full script for case 2.2 is located in benchmarks/davies_et_al/case-2.2.prm

## Case 2.3: BA_Ra103_vv_FS.#

Case 2.3 is a variation on the previous one:

Boussinesq Approximation

Boundary Condition: Free-Slip

Rayleigh Number = \(10^3\)

Initial Conditions: Final conditions of case 2.1 (BA_Ra104_Iso_FS)

\(\eta(T) = 1000^{-T}\)

The Rayleigh number is smaller here (and is selected using the gravity
parameter in the input file, as before), but the more important change is that
the viscosity is now a function of temperature. At the time of writing, there
is no material model that would implement such a viscosity, so we create a
plugin that does so for us (see Extending and contributing to ASPECT and
How to write a plugin in general, and
Material models for material models in particular).
The code for it is located in
benchmarks/davies_et_al/case-2.3-plugin/VoT.cc (where “VoT” is
short for “viscosity as a function of temperature”) and is
essentially a copy of the `simpler`

material model. The primary change
compared to the `simpler`

material model is the line about the viscosity in
the following function:

```
template <int dim>
void
VoT<dim>::
evaluate(const typename Interface<dim>::MaterialModelInputs &in,
typename Interface<dim>::MaterialModelOutputs &out) const
{
for (unsigned int i=0; i<in.position.size(); ++i)
{
out.viscosities[i] = eta*std::pow(1000,(-in.temperature[i]));
out.densities[i] = reference_rho * (1.0 - thermal_alpha * (in.temperature[i] - reference_T));
out.thermal_expansion_coefficients[i] = thermal_alpha;
out.specific_heat[i] = reference_specific_heat;
out.thermal_conductivities[i] = k_value;
out.compressibilities[i] = 0.0;
}
}
```

Using the method described in Sections Running benchmarks that require code and How to write a plugin, and the files in the benchmarks/davies_et_al/case-2.3-plugin, we can compile our new material model into a shared library that we can then reference from the input file. The complete input file for case 2.3 is located in benchmarks/davies_et_al/case-2.3.prm and contains among others the following parts:

```
set Additional shared libraries = ./case-2.3-plugin/libVoT.so
subsection Material model
set Model name = VoT
subsection VoT model
set Reference density = 1
set Reference specific heat = 1.
set Reference temperature = 0
set Thermal conductivity = 1
set Thermal expansion coefficient = 1e-5
set Viscosity = 1
end
end
```

## Results.#

In the following, let us discuss some of the results of the benchmark setups discussed above. First, the final steady state temperature fields are shown in Fig. 201. It is immediately obvious how the different Rayleigh numbers affect the width of the plumes. If one imagines a setup with constant gravity, constant inner and outer temperatures and constant thermal expansion coefficient (this is not how we describe it in the input files, but we could have done so and it is closer to how we intuit about fluids than adjusting the gravity), then the Rayleigh number is inversely proportional to the viscosity – and it is immediately clear that larger Rayleigh numbers (corresponding to lower viscosities) then lead to thinner plumes. This is nicely reflected in the visualizations.

Secondly, Fig. 202 shows the root mean square velocity as a function of time for the various cases. It is obvious that they all converge to steady state solutions. However, there is an initial transient stage and, in cases 2.2 and 2.3, a sudden jolt to the system at the time where we switch from the model used to compute up to time \(t=2\) to the different models used after that.

These runs also produce quantitative data that will be published along with the concise descriptions of the benchmarks and a comparison with other codes. In particular, some of the criteria listed above to judge the accuracy of results are listed in Table 10.[1]

Case |
\(\left<T\right>\) |
\(Nu_T\) |
\(Nu_B\) |
\(V_{\text{rms}}\) |
---|---|---|---|---|

1.1 |
0.403 |
2.464 |
2.468 |
19.053 |

2.1 |
0.382 |
4.7000 |
4.706 |
46.244 |

2.2 |
0.382 |
9.548 |
9.584 |
193.371 |

2.3 |
0.582 |
5.102 |
5.121 |
79.632 |