首页> 外文期刊>Modern Physics Letters, B. Condensed Matter Physics, Statistical Physics, Applied Physics >Investigation of turbulence-induced quadrupole source acoustic characteristics of a three-dimensional hydrofoil
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Investigation of turbulence-induced quadrupole source acoustic characteristics of a three-dimensional hydrofoil

机译:三维水翼湍流诱导的四维水源声源声学特性研究

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In order to investigate the turbulence-induced acoustic characteristics of hydrofoils, the flow and sound field for a model NH-15-18-1 asymmetric hydrofoil were calculated based on the mixed method of large eddy simulation (LES) with Lighthill analogy theory. Unsteady fluid turbulent stress source around the hydrofoil were selected as the inducements of quadrupole sound. The average velocity along the mainstream direction was calculated for different Reynolds numbers (Re). Compared to experimental measurements, good agreement was seen over a range of Re. The results showed that the larger the Re, the larger the vortex intensity, the shorter the vortex initial shedding position to the leading edge of the hydrofoil, and the higher the vortex shedding frequency (f(s)). The maximum sound pressure level (SPL) of the hydrofoil was located at the trailing edge and wake of the hydrofoil, which coincided with the velocity curl (omega) distribution of the flow field. The maximum SPL of the sound field was consistent with the location of the vortex shedding. There were quadratic positive correlations between the total sound pressure level (TSPL) and the maximum value of the vortex intensity (Gamma(max)) and velocity curl, which verified that shedding and diffusion of vortices are the fundamental cause of the generation of the quadrupole source noise.
机译:为了研究水翼轴的湍流引起的声学特性,基于Lighthill类比理论的大型涡模拟(LES)的混合方法计算了NH-15-18-1不对称水翼仪的流动和声场。水翼罐周围的不稳定流体湍流应力源作为四极声的诱导。为不同的雷诺数(RE)计算了沿着主流方向的平均速度。与实验测量相比,在一系列RE中看到了良好的一致。结果表明,RE越大,涡强度越大,涡流初始脱落位置越短到水翼的前缘,涡流脱落频率越高(F(S))。水翼罐的最大声压水平(SPL)位于水翼的后缘和尾部,这与流场的速度卷曲(Ω)分布一致。声场的最大SEC与涡旋脱落的位置一致。总声压水平(TSPL)与涡旋强度的最大值(伽马(最大))和速度卷曲之间存在二次正相关性,验证了换流和涡流的扩散是四极的产生的根本原因源噪声。

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