Experimental Investigation Of The Acoustic Signature Of A Quad-Rotor Evtol Aircraft In Hover

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dc.contributor.authorBucherelli, G.
dc.contributor.authorDas, L.
dc.contributor.authorGrassi, D.
dc.contributor.authorGranata, D.
dc.contributor.authorZanotti, A.
dc.date.accessioned2026-08-14T09:30:17Z
dc.date.issued2025
dc.description.abstractThe present study aims at providing a proper aeroacoustic characterization of the single-passenger configuration of the quadrotor concept vehicle designed by NASA, through an experimental campaign in the new anechoic chamber at Politecnico di Milano. A scaled model of the quadrotor CRM was designed from scratch and manufactured to be exploited to collect aerodynamic force and acoustic measurements in hover condition, with a particular focus on rotor-on-rotor interaction phenomena by adopting a breakdown approach where rotors were progressively added.
dc.identifier.citation51st European Rotorcraft Forum (ERF 2025), September 9-12, 2025, Venice, Italy : proceeedings. ISBN 9798331335472.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4770
dc.language.isoen
dc.titleExperimental Investigation Of The Acoustic Signature Of A Quad-Rotor Evtol Aircraft In Hover

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