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EFFECT OF SPACING BETWEEN THE PUSHER PROPELLER AND WING ON ENVIRONMENTAL LIGHT AIRCRAFT NOISE

卷 47, 册 6, 2016, pp. 639-647
DOI: 10.1615/TsAGISciJ.2017019465
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摘要

This paper presents the results of an experimental study on the effect of the spacing between the pusher propeller and the wing located in front of it on the environmental noise produced by a light aircraft. It is shown that increasing the axial spacing by 0.1 m yields a 4.6 dBA reduction in the environmental noise by reducing the intensity of the radiation at the harmonics of the blade passing frequency. If the axial spacing exceeds the wing chord (pylon, fin), the effect of the propeller placement in the pusher arrangement disappears and the propeller noise in the given configuration becomes comparable with the noise of an isolated propeller.

对本文的引用
  1. A. Moshkov P., F. Samokhin V., A. Yakovlev A., Engine-propeller power plant aircraft community noise reduction key methods, 1952, 2018. Crossref

  2. Moshkov Petr, Study of the influence of in-flight conditions on the light propeller-driven aircraft noise, Aerospace Systems, 5, 1, 2022. Crossref

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