Airfoil trailing-edge noise source identification using large-eddy simulation and wavelet transform

Seongkyu Lee, Donghun Kang, Davy Joao Etienne Brouzet +1

Airfoil noise is predicted and analyzed using wall-resolved large-eddy simulations and wavelet transforms for a NACA 0012 airfoil at a Mach number of 0.06 and a Reynolds number of…