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Mechanisms of jet noise generation: classical theories and recent developments

机译:喷气噪声产生的机理:经典理论和最新进展

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Lighthill's acoustic analogy and several variants of it have been used to interpret, analyze and explain measured data. In this paper, the validity of the main tenets of the classical theories is examined. This assessment is facilitated by a new comprehensive aeroacoustic database. The overall sound power level does not exactly follow the eighth power of velocity (Vj/a), but has a weak dependence on jet temperature. It has been believed that an additional source of noise, with either sixth or fourth power variation with velocity, appears for heated jets; there is also a supposed change in spectral shape at 90°, even though effects associated with convection and flow/acoustic interaction are negligible at that angle. The new data indicate that the velocity exponent for overall power is close to eight even at a very high stagnation temperature ratio of 3.2. Moreover, the spectral shape is invariant with jet Mach number and jet temperature. A careful assessment of Tanna's database, which provided the rationale and justification for many of the theoretical models, reveals that this database is unreliable and exhibits incorrect spectral trends. A fundamental tenet of the classical theories, based on both the formalisms of Lighthill-Ffowcs Williams and Lilley, is the notion of moving sources. This idea immediately leads to a Doppler shift for frequency and a convective amplification factor for the noise radiated to the aft angles. It is demonstrated with the new database that there is no experimental evidence for these conjectured effects of moving sources. The jet temperature ratio (static or stagnation), in addition to jet velocity Vj/a, is an independent controlling parameter. New scaling laws that are valid for all angles have been developed with the current database. There are no multiplicative factors with adjustable constants for the spectrum functions; the spectrum function and the velocity exponent depend on the jet temperature ratio and the radiation angle. This relation represents the main difference between the current and the classical formulations. A single exponent collapses the entire spectrum from jets with different Vj/a, but at fixed jet temperature ratio. Therefore, there is no experimental evidence for the main classical ideas of jet noise, as consisting of multipoles and moving sources, as they are inconsistent with the new data. The idea of two distinct sources that are related to the fine-scale and large-scale turbulence of the jet plume has been investigated. Experimental evidence for the importance of the noise from large coherent structures even at low velocities is offered. The observation at lower and large aft angles of distinct characteristics in, (1) the far field spectral shapes, (2) the directivities of the peak Strouhal number and the OASPL, (3) the directivity of the velocity exponent, and (4) the polar and azimuthal correlations of the farfield pressure, provides strong evidence to support the above view of two different sources of jet noise.
机译:Lighthill的声学比喻及其多种变体已用于解释,分析和解释测量数据。本文研究了古典理论主要思想的有效性。新的综合航空声学数据库促进了这一评估。总体声功率级不完全符合速度的八次方(V j / a),但对射流温度的依赖性很小。可以相信,加热射流会出现一个附加的噪声源,该噪声源具有随速度变化的第六或第四功率。即使在该角度下与对流和流/声相互作用相关的影响可以忽略不计,在90°处的光谱形状也会发生变化。新数据表明,即使在3.2的极高停滞温度比下,总功率的速度指数也接近于8。此外,光谱形状随射流马赫数和射流温度而不变。对Tanna数据库的仔细评估(为许多理论模型提供了理论依据和合理性)表明,该数据库不可靠,并且频谱趋势不正确。基于Lighthill-Ffowcs Williams和Lilley的形式主义的古典理论的基本原则是移动源的概念。这个想法立即导致频率的多普勒频移和辐射到后角的噪声的对流放大因子。新的数据库证明,没有实验证据证明这些移动源会产生这些推测的影响。除射流速度V j / a外,射流温度比(静态或停滞)是一个独立的控制参数。当前数据库已开发出对所有角度均有效的新缩放定律。对于频谱函数,没有常数可调的乘法因子。谱函数和速度指数取决于射流温度比和辐射角。这种关系代表了当前公式与经典公式之间的主要区别。一个单一的指数会使具有不同V j / a的射流的整个光谱崩溃,但射流温度比是固定的。因此,对于由多极点和运动源组成的射流噪声的主要经典观点,没有实验证据,因为它们与新数据不一致。已经研究了与喷射烟流的细尺度和大尺度湍流有关的两种不同来源的想法。实验证明,即使在低速下,来自大型相干结构的噪声也很重要。在较低和较大的后角观察到的独特特征包括:(1)远场光谱形状;(2)斯特劳哈尔峰峰值和OASPL的方向性;(3)速度指数的方向性;(4)远场压力的极坐标和方位角相关性提供了有力的证据来支持上述两种不同的射流噪声源的观点。

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