Characterization of pressure fluctuations within a controlled-diffusion blade boundary layer using the equilibrium wall-modelled LES
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DOI: 10.1038/s41598-020-69671-y
Abstract: In this study, the generation of airfoil trailing edge broadband noise that arises from the interaction of turbulent boundary layer with the airfoil trailing edge is investigated. The primary objectives of this work are: (i)… read more here.
Keywords: wall modelled; controlled diffusion; edge; boundary layer ... See more keywords