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CALCULATION OF BASIC SOUND RADIATION OF AXISYMMETRIC JETS BY DIRECT NUMERICAL SIMULATIONS

机译:直接数值模拟计算轴对称飞机的基本声辐射

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The basic radiation of sound from forced laminar axisymmetric jets(Re_D =6 x 10~2 to 1.5 x 10~3 ) is calculated by a hybrid approach, whereby the hydrodynamic field is calculated by an incompressible stream function-vorticity direct numerical simulation(DNS) and the sound field is calculated by the compact Lighthill and Mohring-Kambe formulations. It is shown that, because fo the oscillatory behavior of the source as a wave packet ,the acoustic results are more sensitive to numerical constraints such as the DNS box size than are the hydrodynamic results. Lighthill's formulation shows a strong sensitivity to the radial boundary condition imposed on the velocity in the DNS. A zero second-order radial derivative for the stream function behaves the best, and a zero radial velocity condition behaves the worst. The Mohring-Kambe formulation shows a strong dependence on the arbitrary location of the coordinate origin. A boundary correction developed to climinate this dependence is shown to work well by achieving a good agreement between the two formulations in the dominant features of the sound radiation. The effects of the inflow momentum thickness and Reynolds number are investigated with reference to the directivity and frequency spectrum of the emitted sound.
机译:通过混合方法计算强制层流轴对称射流的基本声辐射(Re_D = 6 x 10〜2至1.5 x 10〜3),从而通过不可压缩的流函数-涡度直接数值模拟(DNS)计算流体动力场),并通过紧凑的Lighthill和Mohring-Kambe公式来计算声场。结果表明,由于声源作为波包的振荡行为,与水动力结果相比,声学结果对数值约束(例如DNS箱尺寸)更加敏感。 Lighthill的公式显示出对DNS速度所施加的径向边界条件的强烈敏感性。流函数的零二阶径向导数表现最佳,而径向速度条件零则表现最差。 Mohring-Kambe公式显示出强烈依赖于坐标原点的任意位置。通过消除声辐射的主要特征中的两个公式之间的良好一致性,可以证明消除这种依赖性的边界校正效果很好。参考流入声音的方向性和频谱,研究了流入动量厚度和雷诺数的影响。

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