The frame change interfaces model the interface between a rotating assembly and a stationary assembly. For details, see Frame Change/Mixing Model in the CFX-Solver Modeling Guide. When the analysis type is steady state, four options are available to model frame change:
None
Stage
: For details, see Stage (Mixing Plane) in the CFX-Solver Modeling Guide.Periodic
Frozen Rotor
: For details, see Frozen Rotor in the CFX-Solver Modeling Guide.
For transient or Transient Blade Row simulations, the following four options are available to model frame change:
None
Stage
: For details, see Stage (Mixing Plane) in the CFX-Solver Modeling Guide.Periodic
Transient Rotor-Stator
: For details, see Transient Rotor-Stator in the CFX-Solver Modeling Guide.
In addition, a frame change interface of type None
is created for tip clearance regions and disconnected regions of
mesh within a component (for example between an inlet section and
a blade section). Periodic interfaces are used in regions where a
portion of the flow field is repeated in many identical regions. The
flow around a single turbine blade in a rotating machine, or around
a single louvre in a whole array in a heat exchanger fin are such
examples.