2
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Map the solution from the CFD mesh to the acoustics mesh. This is done by using the Transient Mapping study step. The input to this study step is only the Time step Δt used in the LES/DES study. In the Transient Mapping study step it is only the Aeroacoustic Flow Source Coupling that is solved for.
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3
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Transform the mapped flow sources to the frequency domain using the Time to Frequency FFT study step. In the Study Settings for the study step, the End time is set to Tend and Maximum output frequency is set to fmax. In the Time to Frequency FFT study step it is also only the Aeroacoustic Flow Source Coupling that is solved for.
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4
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Finally, solve the acoustic problem in the frequency domain. In the Frequency Domain study step it is only the Pressure Acoustics, Frequency Domain physics that is solved for. The Values of variables not solved for settings should point to the Time to Frequency FFT study.
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Cavity Flow Noise tutorial available in the COMSOL Application Gallery at: https://www.comsol.com/model/cavity-flow-noise-105021
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For further details about LES and DES see the CFD Module User’s Guide:
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