Boundary layer parameters extraction in ADFlow

[luigimanni]

Dear all,

I have performed a CFD analysis on a 2D airfoil on ADflow, and I now need to perform an aeroacoustic evaluation of the airfoil using a Trailing Edge Noise (TEN) code.

The inputs of the TEN code are the following boundary layer parameters, extracted text to the trailing edge:

• BL thickness (99%)
• BL displacement thickness
• BL momentum thickness
• Momentum thickness Reynolds number

Can anyone suggest me how to extract these properties from the simulation on ADFLOW?

Thank you very much in advance.