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Adaptation of the Azimuthal Decomposition Technique to Jet Noise Measurements in Full-Scale Tests

机译:方位角分解技术在全面测试中对射流噪声测量的适应性

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摘要

To develop jet noise-reduction concepts, it is necessary to understand the physics underlying the noise-generation process. Decomposition of the sound field into azimuthal modes is one of the effective experimental methods that allows extracting subtle features of different types of noise sources. For turbulent flows, the interpretation of the noise analysis results using the azimuthal decomposition technique was developed by the authors in previous papers. In the present paper, a generalization of this method allowing the decomposition of the jet acoustic field into azimuthal modes by means of reduced number of microphones is developed. It is shown that jet noise measurements by only three microphones in each cross section allow reconstruction of three azimuthal mode directivities (axisymmetric, first, and second) for both low and moderate frequency bands. Furthermore, two-microphone measurements, provided the microphones are properly located, make it possible to reconstruct directivity of the axisymmetric mode and total directivity of the first and second modes. The latter method is shown to be suitable for using with an outdoor test bench. The modified methodology is first validated on a small-scale laboratory database. Next, it is applied to the jet of a real engine in ground tests. The information about the azimuthal modes properties may be used to investigate physical aspects of the large-scale jet noise sources.
机译:为了发展减少喷气噪声的概念,有必要了解噪声产生过程背后的物理原理。将声场分解为方位角模式是一种有效的实验方法,可以提取不同类型噪声源的细微特征。对于湍流,作者在先前的论文中开发了使用方位角分解技术对噪声分析结果的解释。在本文中,开发了这种方法的一般化,该方法允许通过减少麦克风的数量将射流声场分解为方位模。结果表明,在每个横截面中只有三个麦克风的喷射噪声测量结果允许针对低频段和中频段重构三个方位模式的方向性(轴对称,第一和第二)。此外,如果麦克风正确放置,则两个麦克风的测量值可以重构轴对称模式的方向性和第一和第二模式的总方向性。已显示后一种方法适合与室外测试台一起使用。修改后的方法首先在小型实验室数据库中得到验证。接下来,在地面测试中将其应用于真实引擎的喷嘴。有关方位模态特性的信息可用于研究大规模喷射噪声源的物理方面。

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  • 来源
    《AIAA Journal》 |2017年第2期|572-584|共13页
  • 作者单位

    Perm Natl Res Polytech Univ, Lab Noise Generat Mech & Modal Anal, Perm 614990, Russia;

    Perm Natl Res Polytech Univ, Lab Noise Generat Mech & Modal Anal, Perm 614990, Russia;

    TsAGI Moscow Branch, Acoust Dept, Moscow 105005, Russia;

    TsAGI Moscow Branch, Acoust Dept, Moscow 105005, Russia;

    Aviadvigatel OJSC, Dept Exhaust Syst & Nacelles, Perm 614990, Russia;

    Aviadvigatel OJSC, Dept External Engine Characterist, Perm 614990, Russia;

    Aviadvigatel OJSC, Dept External Engine Characterist, Perm 614990, Russia;

    Aviadvigatel OJSC, Dept External Engine Characterist, Perm 614990, Russia;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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