Browsing Waterloo Research by Subject "low Reynolds number airfoil"
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Computational Aeroacoustic Prediction of Tonal Noise for Low Reynolds Number Airfoils
(American Institute of Aeronautics and Astronautics, 2024-05-30)Airfoils operating in low Reynolds number, Re, conditions can generate tonal aeroacoustic noise due to the laminar or transitional boundary layer (BL) at the airfoil trailing edge (TE). At modest Re of less than 1×10⁵, an ...