Experiments and modeling of perpendicular cylinder-airfoil interaction show acoustic output driven by cylinder-wake coherent structures at St=0.38, with reasonable agreement from linearised Powell-Howe source terms and a proposed spanwise Fourier-mode model.
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Perpendicular rod-airfoil aeroacoustics: experiments and modelling of interaction noise
Experiments and modeling of perpendicular cylinder-airfoil interaction show acoustic output driven by cylinder-wake coherent structures at St=0.38, with reasonable agreement from linearised Powell-Howe source terms and a proposed spanwise Fourier-mode model.