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

机译:直接数值模拟研究休克/各向同性湍流相互作用噪声研究

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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:进行了相结合灯灰声学类比的冲击/各向同性湍流相互作用的直接数值模拟,首次研究了震动/湍流相互作用(STI)对本文湍流噪声的影响。 STI仿真的上游马赫数和上游湍流Mach编号分别为1.29和0.05。基于数值模拟结果,在STI下,低频带中的功率谱密度略微增加,高频带中的值明显增加。因此,声强度由STI放大。通过分析湍流流场和声场,发现各向同性上游湍流成为正常冲击波的一维压缩下的轴对称湍流。通过根据不同的噪声源将声压分解成六个部分,鉴定了本文中观察点的主要噪声源。主源由横向方向上的正常应力构成。另外,本文湍流强度较弱,导致主要噪声源被简化为正常应力的密度和二阶时间衍生的产生。 STI下的噪声变化机制可分为两部分。首先,冲击波的压缩效果增加了下游密度。其次,STI在整个波数范围内增加湍流动力谱。

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