5.13 Steady-state convergence
The absence of a time derivative from an
equation written in steady-state form reduces the diagonal
dominance, and hence convergence, of the resulting matrix equation,
as discussed in Sec. 5.5
. Under-relaxation is
therefore applied to
, and
to promote convergence in the algorithm in
Sec. 5.12
.
The and
fields use equation under-relaxation with
factors
and
, respectively. A value of 0.7 is commonly applied,
decreasing to 0.5 for less convergent cases (and sometimes to 0.3
in compressible flow cases, beyond the scope of this book).
Under-relaxation of is more subtle. The
flux corrector requires that
is not under-relaxed
to ensure
obeys mass conservation better. For the momentum corrector,
field under-relaxation is subsequently applied to
with a factor
.
To find an optimal
for the momentum corrector, we examine
![]() |
(5.22) |




Convergence is compromised by the explicit nature
of . It can be more implicit by “adding and subtracting”
,
where coefficients
are applied to
in the “owner”
cells:
![]() |
(5.23) |
![]() |
(5.24) |

![]() |
(5.25) |









![]() |
(5.26) |


Residual control
The algorithm in Sec. 5.12
uses a fixed number of solution
steps . In practice,
must be chosen to be large enough to reach an
acceptable level of convergence. Once convergence is reached, the
simulation should stop to avoid unnecessary computing cost.
A common stopping criterion applies a residual level for each equation, below which the equation is deemed to be converged. When all equations satisfy their respective residual controls, the simulation then stops.
Convergence can also be determined by monitoring any suitable metric, including objective measurements from the simulation, e.g. a force coefficient. When the metric no longer changes significantly over subsequent steps, the simulation is stopped.