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• W4387132132 abstract "We investigate the aerodynamic and aeroacoustic characteristics of a small-scale drone rotor operating in axial descending flight. The integrated aerodynamic forces and the far-field noise are measured by wind tunnel experiments. Then, near-field flow structures and corresponding noise source analysis are presented based on computational aeroacoustics (CAA) simulations. We found the unique acoustic feature of descending flight is the haystacking-like spectral humps, possibly caused by the interaction between the blade leading edge and the rotor wake." @default.
• W4387132132 created "2023-09-29" @default.
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• W4387132132 date "2023-09-28" @default.
• W4387132132 modified "2023-09-29" @default.
• W4387132132 title "Experimental and numerical investigations on rotor noise in axial descending flight" @default.
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• W4387132132 doi "https://doi.org/10.1103/physrevfluids.8.094803" @default.
• W4387132132 hasPublicationYear "2023" @default.
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