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Investigation on Noise from Shock/Isotropic Turbulence Interaction Using Direct Numerical Simulation

机译:直接数值模拟研究冲击/各向同性湍流相互作用产生的噪声

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Direct numerical simulation of shock/isotropic turbulence interaction combining Lighthill acoustic analogy is conducted to study the influence of shock/turbulence interaction (STI) on the turbulence noise in this paper, for the first time. The upstream Mach number and upstream turbulent Mach number for STI simulation are 1.29 and 0.05 respectively. Based on the numerical simulation results, Power Spectral Density in the low frequency band is slightly increased under STI and the value in the high frequency band is obviously increased. Therefore, the acoustic intensity is amplified by STI. By analyzing the turbulent flowfield and the acoustic field, it is found that the isotropic upstream turbulence becoming axisymmetric turbulence under the one-dimensional compression of the normal shock wave. By decomposing the acoustic pressure into six parts according to different noise sources, the primary noise sources for the observation points in this paper are identified. The primary sources are constituted by the normal stresses in the transverse directions. Additionally, the turbulence intensity is weak in this paper, resulting in the primary noise sources being simplified as the production of density and second order time derivative of the normal stress. The mechanisms of noise variation under STI can be divided into two parts. First, the compression effect of shock wave increases the downstream density. Second, STI increases the turbulent kinetic energy spectrum over the entire wavenumber range.
机译:本文首次结合Lighthill声学模拟方法对冲击/各向同性湍流相互作用进行了直接数值模拟,以研究冲击/湍流相互作用(STI)对湍流噪声的影响。 STI模拟的上游马赫数和上游湍流马赫数分别为1.29和0.05。根据数值模拟结果,在STI下低频段的功率谱密度略有增加,而高频段的值则明显增加。因此,声强度被STI放大。通过分析湍流场和声场,发现各向同性上游湍流在法向冲击波的一维压缩作用下变成轴对称湍流。通过根据不同的噪声源将声压分解为六个部分,确定了本文观测点的主要噪声源。主要来源由横向的法向应力构成。此外,本文的湍流强度较弱,导致主要噪声源简化为法向应力的密度和二阶时间导数的产生。 STI下的噪声变化机制可分为两部分。首先,冲击波的压缩作用增加了下游密度。其次,STI增加了整个波数范围内的湍动能谱。

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