Direct Noise Calculation
Direct noise calculation, or the Computational Aeroacoustics approach, requires solving the entire flow field for the full unsteady simulation.
To calculate the aerodynamically generated acoustics, record the time-varying static pressure on points (probes) or surfaces. It requires high numerical resolution to capture the spatial and transient effects of the acoustic pressure perturbations. For post-processing, the Fourier Transform (FT) tools can be used for spectral analysis. (See the section on data set functions for details.).
Predicting noise levels near to the source of sound generation can be done directly within a CFD model. Direct simulation can be too expensive to predict noise levels some distance from the source, however. For such far-field predictions, Simcenter STAR-CCM+ provides the Ffowcs Williams-Hawkings (FW-H) acoustics integral formulation.