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An investigation of the noise field from a small jet and methods for its reduction.

机译:对小型喷气机噪声场的研究及其减少方法。

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摘要

Sound measurements have been made on the noise from the jet of a one inch diameter convergent nozzle at atmospheric temperature and at speeds above and below choking. The noise level and spectrum have been investigated in both the near and distant fields. The results agree in some measure with the predictions of the Lighthill theory, that the elementary sound radiator is an acoustic quadrupole. The agreement is more marked if attention is confined to the higher frequencies.Simple empirical formulae are derived giving the overall sound intensity and frequency spectrum in terms of the position relative to the jet, the stagnation pressure excess over the atmospheric pressure, and the frequency.The results of tests on various noise reduction devices are discussed. These tests indicate promising lines of investigation. The maximum reduction in total noise level was about 10 db.
机译:在大气温度下,以高于或低于窒息的速度,对一英寸直径的收敛喷嘴的射流产生的噪声进行了声音测量。已经在近场和远场中研究了噪声水平和频谱。结果在某种程度上与Lighthill理论的预测相符,即基本声辐射器是声四极杆。如果将注意力集中在较高的频率上,则该协议更加明显。得出了简单的经验公式,给出了相对于射流的位置,相对于大气压的滞止压力过剩以及频率而言的总体声音强度和频谱。讨论了各种降噪设备的测试结果。这些测试表明有希望的研究方向。总噪声水平的最大降低约为10 db。

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  • 作者

    Westley R.; Lilley G. M.;

  • 作者单位
  • 年度 1952
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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