Replaced the ad hoc geometric mean blending with the more physical wall distance
Reynolds number blending function.
Additionally the part of the production term active for y+ < 11.6 has been
reinstated.
Sets the boundary values of p_rgh corresponding to a constant density hydrostatic
pressure distribution.
Description
This boundary condition provides a hydrostatic pressure condition for p_rgh,
calculated as:
\f[
p_{rgh} = p_{ref} - (\rho - \rho_0) g (h - h_{ref})
\f]
where
\vartable
p_{rgh} | Pseudo hydrostatic pressure [Pa]
p_{ref} | Static pressure at hRef [Pa]
h | Height in the opposite direction to gravity
h_{ref} | Reference height in the opposite direction to gravity
\rho | Density field
\rho_{ref} | Uniform reference density at boundary
g | Acceleration due to gravity [m/s^2]
\endtable
Usage
\table
Property | Description | Required | Default value
pRef | Reference static pressure | yes |
rhoRef | Reference density | yes |
rho | Density field name | no | rho
\endtable
Example of the boundary condition specification:
\verbatim
<patchName>
{
type prghUniformDensityHydrostaticPressure;
rhoRef 1000;
p 0;
value uniform 0; // optional initial value
}
\endverbatim
Partial elimination has been implemented for the multiphase Euler-Euler
solver. This does a linear solution of the drag system when calculating
flux and velocity corrections after the solution of the pressure
equation. This can improve the behaviour of the solution in the event
that the drag coupling is high. It is controlled by means of a
"partialElimination" switch within the PIMPLE control dictionary in
fvSolution.
A re-organisation has also been done in order to remove the exposure of
the sub-modelling from the top-level solver. Rather than looping the
drag, virtual mass, lift, etc..., models directly, the solver now calls
a set of phase-system methods which group the different force terms.
These new methods are documented in MomentumTransferPhaseSystem.H. Many
other accessors have been removed as a consequence of this grouping.
A bug was also fixed whereby the face-based algorithm was not
transferring the momentum associated with a given interfacial mass
transfer.
Description
Evaluates and writes the turbulence intensity field 'I'.
The turbulence intensity field 'I' is the root-mean-square of the turbulent
velocity fluctuations normalised by the local velocity magnitude:
\f[
I \equiv \frac{\sqrt{\frac{2}{3}\, k}}{U}
\f]
To avoid spurious extrema and division by 0 I is limited to 1 where the
velocity magnitude is less than the turbulent velocity fluctuations.
Example of function object specification:
\verbatim
functions
{
.
.
.
turbulenceIntensity
{
type turbulenceIntensity;
libs ("libfieldFunctionObjects.so");
}
.
.
.
}
\endverbatim
or using the standard configuration file:
\verbatim
functions
{
.
.
.
#includeFunc turbulenceIntensity
.
.
.
}
\endverbatim
This change means that getApplication still works if we have a
controlDict.orig, rather than a controlDict. This allows us to simplify
the scripting of tutorials in which the controlDict is modified.
Minmod is the default limiter function and specified with an explicit name e.g.:
gradSchemes
{
default Gauss linear;
limited cellLimited Gauss linear 1;
}
Venkatakrishnan and cubic limiter functions are also provided and may be
specified explicitly e.g.:
gradSchemes
{
default Gauss linear;
limited cellLimited<Venkatakrishnan> Gauss linear 1;
}
or
gradSchemes
{
default Gauss linear;
limited cellLimited<cubic> 1.5 Gauss linear 1;
}
The standard minmod function is recommended for most applications but if
convergence or stability problems arise it may be beneficial to use one of the
alternatives which smooth the gradient limiting. The Venkatakrishnan is not
well formulated and allows the limiter to exceed 1 whereas the cubic limiter is
designed to obey all the value and gradient constraints on the limiter function,
see
Michalak, K., & Ollivier-Gooch, C. (2008).
Limiters for unstructured higher-order accurate solutions
of the Euler equations.
In 46th AIAA Aerospace Sciences Meeting and Exhibit (p. 776).
The cubic limiter function requires the transition point at which the limiter
function reaches 1 is an input parameter which should be set to a value between
1 and 2 although values larger than 2 are physical but likely to significantly
reduce the accuracy of the scheme.
The tutorial demonstrates generation of a C-grid mesh using blockMesh
The geometry is provided by a surface mesh (OBJ file) of the NACA0012 aerofoil
The case is setup with a freestream flow speed of Ma=0.72
Thanks to Kai Bastos at Duke University for the geometry and helpful input.
Some tutorials have had Allrun scripts added in order to run setFields,
which was previously omitted. Others have had nonuniform field files in
the 0 directory replaced by uniform files with .orig extensions.
These BCs blend between typical inflow and outflow conditions based on the
velocity orientation.
airFoil2D tutorial updated to demonstrate these new BCs.
Without -fields specified mergeOrSplitBaffles now manipulates the mesh only and
with the -fields option also updates the fields corresponding to the mesh change.
Now if a <field> file does not exist first the compressed <field>.gz file is
searched for and if that also does not exist the <field>.orig file is searched
for.
This simplifies case setup and run scripts as now setField for example can read
the <field>.orig file directly and generate the <field> file from it which is
then read by the solver. Additionally the cleanCase function used by
foamCleanCase and the Allclean scripts automatically removed <field> files if
there is a corresponding <field>.orig file. So now there is no need for the
Allrun scripts to copy <field>.orig files into <field> or for the Allclean
scripts to explicitly remove them.
