The Aeroacoustic Flow Source feature is used to set up aeroacoustic flow-induced noise sources in the pressure acoustics model. The feature is best used when coupling to a
Fluid Flow model (LES, DES, or RANS-EVM SST-SAS) or to
The Imported Fluid Flow Interface, using the
Aeroacoustic Flow Source Coupling and the dedicated
Transient Mapping study. The feature only exists in 3D. The feature can also be used with user-defined expressions for a Lighthill like source expressed in terms of a stress tensor
Tij (SI unit: N/m
2). Add this node from the
More submenu.
Select the Acoustic analogy as
Lighthill (the default) or
Aeroacoustic wave equation. The
Domain Section and the
Boundary Selection should match the corresponding selections made in the
Aeroacoustic Flow Source Coupling multiphysics node.
When the multiphysics coupling is used, the Stress tensor (
T),
Normal mass flow on exterior boundaries (
mn), or the
Flow pressure variation, second time derivative (

) field are automatically coupled (appear grayed out).
To use a window function click and select Use window function, the default expression is 1 which corresponds to not having a window. When selected enter an expression for the
Window function w(
x). The function should be a spatially varying expression that smoothly truncates the computational domain. Example of window or truncation functions are given in
Ref. 76 and
Ref. 77.