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publicationDate 2020-11-10-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-10829206-B2
titleOfInvention Wing leading edge features to attenuate propeller wake-wing acoustic interactions
abstract An apparatus configured to reduce acoustic interactions between a propeller and a surface of an aircraft positioned downstream of the propeller includes a surface modification element of the surface of the aircraft. The surface modification element defines a modified contour of the surface. The modified contour is configured to decorrelate a phase distribution of a plurality of sound sources within a source field positioned on at least a portion of the surface.
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