{
  "id": "2202.13936",
  "version": "v1",
  "published": "2022-02-28T16:41:42.000Z",
  "updated": "2022-02-28T16:41:42.000Z",
  "title": "Sound from rotors near a trailing edge",
  "authors": [
    "Michael Carley"
  ],
  "categories": [
    "physics.flu-dyn"
  ],
  "abstract": "A method of noise reduction proposed for the next generation of aircraft is to shield noise from the propulsion system, by positioning the noise source over a wing or another surface. In this paper, an approximate analysis is developed for the acoustic field far from a circular source placed near the edge of a semi-infinite plate, a model problem for shielding of noise by a wing and for scattering by a trailing edge. The approximation is developed for a source of small radius and is found to be accurate when compared to full numerical evaluation of the field.",
  "revisions": [
    {
      "version": "v1",
      "updated": "2022-02-28T16:41:42.000Z"
    }
  ],
  "analyses": {
    "keywords": [
      "trailing edge",
      "acoustic field far",
      "propulsion system",
      "noise source",
      "full numerical evaluation"
    ],
    "note": {
      "typesetting": "TeX",
      "pages": 0,
      "language": "en",
      "license": "arXiv",
      "status": "editable"
    }
  }
}