The Turbulent Flow, Algebraic yPlus version of the
Rotating Machinery, High Mach Number Flow (hmnf) interface (

), found under the
High Mach Number Flow >
Rotating Machinery, High Mach Number Flow >
Turbulent Flow branch (

), is used to simulate gas flows in geometries with one or more rotating parts and gas at high Reynolds number where the velocity magnitude is comparable to the speed of sound, that is, turbulent flows in the transonic and supersonic range.The physics interface is available for 3D and 2D components and it combines the
High Mach Number Flow, Algebraic yPlus interface (

), with a
Rotating Domain under
Definitions >
Moving Mesh.
There are two study types available for this physics interface. Using the Time Dependent study type, rotation is achieved through moving mesh functionality, also known as sliding mesh. Using the
Frozen Rotor study type, the rotating parts are kept frozen in position, and rotation is accounted for by the inclusion of centrifugal and Coriolis forces. Turbulence effects are included using an enhanced viscosity model based on the local wall distance. The physics interface therefore includes a wall distance equation. The Algebraic yPlus model is a so-called low-Reynolds number model, which means that it can resolve the velocity, pressure, and temperature fields all the way down to the wall. The physics interface also supports heat transfer in solids as well as surface-to-surface radiation.
When this multiphysics interface is added, the following default nodes are also added in the Model Builder under
High Mach Number Flow, Algebraic yPlus —
Fluid,
Initial Values,
Wall, and
Thermal Insulation. When a pair boundary is created, the
Continuity node is automatically added. Then, from the
Physics toolbar, add other nodes that implement, for example, boundary conditions, volume forces, and heat sources. You can also right-click the node to select physics features from the context menu. See
Moving Mesh for more details of the
Rotating Domain node added automatically in the
Model Builder under
Definitions >
Moving Mesh.
The Label is the default physics interface name.
The Name is used primarily as a scope prefix for variables defined by the physics interface. Refer to such physics interface variables in expressions using the pattern
<name>.<variable_name>. In order to distinguish between variables belonging to different physics interfaces, the
name string must be unique. Only letters, numbers, and underscores (_) are permitted in the
Name field. The first character must be a letter.
The default Name (for the first physics interface in the model) is
hmnf.
The Reference temperature Tref is used to define the reference enthalpy
Href which is set to 0 J/kg at
pref (1 atm) and
Tref. When the
Include kinetic energy checkbox is selected, the conservative total-energy equation is solved.
The default Turbulence model type is
RANS-EVM, the default
Turbulence model is
Algebraic yPlus. The
Heat transport turbulence model is implicitly set to
Turbulent Prandtl number. The default
Turbulent Prandtl number model is
Kays–Crawford, which can be changed to
Extended Kays–Crawford or
User-defined turbulent Prandtl number. For
Extended Kays–Crawford, enter a
Reynolds number at infinity Re∞. For
User-defined turbulent Prandtl number, enter a
Turbulent Prandtl number PrT.
The values or expressions required are entered in the Model Inputs section of the
Fluid feature node. For the description of theory of turbulent heat transport see
Turbulent Conductivity.
The dependent variables (field variables) are the Velocity field u (SI unit: m/s), the
Pressure p (SI unit: Pa), and the
Temperature T (SI unit: K). For turbulence modeling,
Reciprocal wall distance G (SI unit: 1/m) and
Wall distance in viscous units yPlus (SI unit: 1) variables are also available.