Selecting an Aeroacoustics Model
To select the Aeroacoustics model:
- In the Physics Model Selection dialog, select a flow model from the Flow group (Coupled Flow or Segregated Flow). The Aeroacoustics radio button becomes available.
-
In the Optional Models group, select
Aeroacoustics.
Following its selection, the Physics Model Selection dialog shows the available aeroacoustics models.
- The Lighthill Stress Tensor model is available with all turbulence models.
- The Ffowcs Williams-Hawkings model is available with both steady and implicit unsteady models.
- The Broadband Noise
Source models are available as follows:
- Curle, Goldstein, and Proudman models can be used in steady and unsteady (transient) analyses. These models are compatible with all Reynolds-Averaged Navier-Stokes (RANS) models that can provide turbulence time and length scales.
- Linearized Euler Equation (LEE) and Lillely Noise Source Model are available only for steady-state simulations. These models can be used with Reynolds-Averaged Navier-Stokes (RANS) cases that include turbulence time and length scales.
- The Acoustic Wave model, the Lighthill Wave model, and the Perturbed Convective Wave model are available for constant density flows with the implicit unsteady model. These aeroacoustics models are not compatible with Explicit, Two-Dimensional, or Axisymmetric models. The Acoustic Wave model and the Lighthill Wave model are compatible with stationary cases only; the simulation cannot include any moving regions (such as fan blades).