The answer is possibly.

But what kind of aeroacoustic problem do you want to tackle?

Stephane Moreau sir I just want to know the effect of sound generation with change in geometry of airfoil and how they are behaving in the far wake zone.

Can you help me by telling how to get the sound data from the already done flow simulation?

What kind of simulation are you running?

The noise comes from the unsteadiness generated on the airfoil.

For instance self-noise which is broadband can only be obtained by LES.

Best regards,

Stéphane

PS: I am referring to turbulent flow based on the Reynolds number based on the chord

Firstly, steady state analysis is needed. The two equation model is usually adopted in the process, and then the transient simulation model is opened after convergence. The LES model is often selected.

Hi, is it possible to use this module for supersonic flow? i seen some of the methods and it is for M