Modeling and simulation of aerodynamic and acoustic installation effects of a small-size quadcopter drone

Multicopter drones are increasingly being used for civil and military applications such as delivery, building inspection, or monitoring. The objective of the project Aeroacoustics for drone PROpulsion (APRO) is to better understand and model the noise-generating mechanisms in multicopter drones in order to reduce their noise impact and to improve their social acceptability. During the first part of the project, experimental setups have been built in the anechoic chamber of ENSTA Paris in order to characterize the aerodynamic performance
and acoustic radiation of isolated propellers and of a small-size quadcopter drone in hover. In a quadcopter drone architecture, several aerodynamic and acoustic installation effects are present that will modify the radiated noise spectrum and directivity with respect to an
isolated propeller configuration. Aerodynamic installation effects are associated to aerodynamic interactions that cause an increase in tonal noise (unsteady loading noise) and potentially in broadband noise too. These installation effects can be associated with the interactions between propellers and their supporting struts, on one side, and the interactions between rotors, on the other side. Acoustic installation effects are associated with the scattering of the propeller noise by the fuselage or other components of the drone, that can yield to amplification or shielding of the noise. Predicting drone noise is thus a complex challenge, especially for small-size drones that operate at relatively low Reynolds numbers, corresponding to transitional regimes on the propeller blades.

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