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?
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:
Can anyone suggest me how to extract these properties from the simulation on ADFLOW?
Thank you very much in advance.