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Wing leading edge features to attenuate propeller wake-wing acoustic interactions
Wing leading edge features to attenuate propeller wake-wing acoustic interactions
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机译:机翼前缘功能可减弱螺旋桨尾流与机翼之间的声音相互作用
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摘要
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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