The RNG -
model was derived using a statistical technique called renormalization
group theory. It is similar in form to the standard
-
model, but includes the following refinements:
The RNG model has an additional term in its
equation that improves the accuracy for rapidly strained flows.
The effect of swirl on turbulence is included in the RNG model, enhancing accuracy for swirling flows.
The RNG theory provides an analytical formula for turbulent Prandtl numbers, while the standard
-
model uses user-specified, constant values.
While the standard
-
model is a high-Reynolds number model, the RNG theory provides an analytically-derived differential formula for effective viscosity that accounts for low-Reynolds number effects. Effective use of this feature does, however, depend on an appropriate treatment of the near-wall region.
These features make the RNG -
model more accurate and reliable for a wider class of flows than the
standard
-
model.
The RNG-based -
turbulence model is derived from the instantaneous Navier-Stokes
equations, using a mathematical technique called "renormalization group" (RNG)
methods. The analytical derivation results in a model with constants different from those in the
standard
-
model, and additional terms and functions in the transport equations for
and
. A more comprehensive description of RNG theory and its application to
turbulence can be found in [499].
The RNG -
model has a similar form to the standard
-
model:
(4–42) |
and
(4–43) |
In these equations, represents the generation of turbulence kinetic energy due to the mean
velocity gradients, calculated as described in Modeling Turbulent Production in the k-ε Models.
is the generation of turbulence kinetic energy due to buoyancy, calculated as
described in Effects of Buoyancy on Turbulence in the k-ε Models.
represents the contribution of the fluctuating dilatation in compressible
turbulence to the overall dissipation rate, calculated as described in Effects of Compressibility on Turbulence in the k-ε Models. The quantities
and
are the inverse effective Prandtl numbers for
and
, respectively.
and
are user-defined source terms.
The scale elimination procedure in RNG theory results in a differential equation for turbulent viscosity:
(4–44) |
where
Equation 4–44 is integrated to obtain an accurate description of how the effective turbulent transport varies with the effective Reynolds number (or eddy scale), allowing the model to better handle low-Reynolds number and near-wall flows.
In the high-Reynolds number limit, Equation 4–44 gives
(4–45) |
with , derived using RNG theory. It is interesting to note that this value of
is very close to the empirically-determined value of 0.09 used in the standard
-
model.
In Ansys Fluent, by default, the effective viscosity is computed using the high-Reynolds number form in Equation 4–45. However, there is an option available that allows you to use the differential relation given in Equation 4–44 when you need to include low-Reynolds number effects.
Turbulence, in general, is affected by rotation or swirl in the mean flow. The RNG model in Ansys Fluent provides an option to account for the effects of swirl or rotation by modifying the turbulent viscosity appropriately. The modification takes the following functional form:
(4–46) |
where is the value of turbulent viscosity calculated without the swirl modification
using either Equation 4–44 or Equation 4–45.
is a characteristic swirl number evaluated within Ansys Fluent, and
is a swirl constant that assumes different values depending on whether the
flow is swirl-dominated or only mildly swirling. This swirl modification always takes effect for
axisymmetric, swirling flows and three-dimensional flows when the RNG model is selected. For
mildly swirling flows (the default in Ansys Fluent),
is set to 0.07. For strongly swirling flows, however, a higher value of
can be used.
The inverse effective Prandtl numbers, and
, are computed using the following formula derived analytically by the RNG
theory:
(4–47) |
where . In the high-Reynolds number limit (
),
.
The main difference between the RNG and standard -
models lies in the additional term in the
equation given by
(4–48) |
where ,
,
.
The effects of this term in the RNG equation can be seen more clearly by rearranging Equation 4–43. Using Equation 4–48, the third and fourth
terms on the right-hand side of Equation 4–43 can be merged, and the
resulting
equation can be rewritten as
(4–49) |
where is given by
(4–50) |
In regions where , the
term makes a positive contribution, and
becomes larger than
. In the logarithmic layer, for instance, it can be shown that
, giving
, which is close in magnitude to the value of
in the standard
-
model (1.92). As a result, for weakly to moderately strained flows, the
RNG model tends to give results largely comparable to the standard
-
model.
In regions of large strain rate (), however, the
term makes a negative contribution, making the value of
less than
. In comparison with the standard
-
model, the smaller destruction of
augments
, reducing
and, eventually, the effective viscosity. As a result, in rapidly strained
flows, the RNG model yields a lower turbulent viscosity than the standard
-
model.
Thus, the RNG model is more responsive to the effects of rapid strain and streamline
curvature than the standard -
model, which explains the superior performance of the RNG model for
certain classes of flows.
The model constants and
in Equation 4–43 have values derived analytically by the
RNG theory. These values, used by default in Ansys Fluent, are