Sponge Layer Model

The Sponge Layer model provides a method for suppressing spurious reflective disturbances near exterior boundaries in direct noise simulations.

Direct noise simulations solve for time-dependent flow variations in compressible fluid flow. These flow variations convect with the flow (for vortical disturbances) or propagate at the speed of sound (for acoustic disturbances) towards the exterior boundaries of the flow domain. For high-quality aeroacoustics simulations, the numerical algorithm must allow these disturbances to travel smoothly through the exterior boundaries without reflecting inside.

Some boundaries, such as the pressure outlet or the stagnation inlet boundary, provide non-reflective conditions. However, the efficiency of non-reflective boundary conditions depends on the inclination angle at which the disturbances reach the boundary—the larger the tangential component of the inclination angle, the less efficient the reflection suppression.

To overcome this dependency on the inclination angle, Simcenter STAR-CCM+ provides the Sponge Layer model, which achieves non-reflective conditions at the boundaries by suppressing unsteady flow variations within a layer of specified thickness—the sponge layer. This volumetric approach prevents the acoustic waves and vortical disturbances from reaching the boundaries and thereby eliminates spurious reflection.