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中文核心期刊

风沙环境下圆柱绕流流动与噪声机理分析

Analysis of flow and noise mechanisms of the flow around a cylinder in windy and sandy environments

  • 摘要: 针对风沙环境下飞机降落阶段噪声突出的关键问题, 开展了Euler-Lagrange方法结合FW-H积分方程的固体颗粒气动噪声混合数值模拟, 研究了风沙环境下的多相流圆柱流场与气动噪声特性。结合涡动力学对比分析了单相与颗粒气固两相圆柱绕流的气动力特性、流动与噪声特性, 探讨了颗粒与旋涡和噪声的作用机制, 揭示了颗粒两相圆柱绕流流动与噪声产生的物理机理。结果表明: 相同来流状态下, 气固两相圆柱绕流的时均阻力系数、表面压力脉动与单相流场相比明显增大; 圆柱前侧颗粒浓度分布呈现出弓状结构的高浓度区, 在该区域有细小涡结构的出现; 颗粒圆柱流场表面压力脉动增加, 并且声源项Lamb矢量散度表征的强涡量与强应变区域相互作用面积增加, 两者共同影响下使得流场噪声增大。

     

    Abstract: In response to the prominent issue of aircraft noise in windy and sandy environments, a numerical method has been applied to combine the Euler-Lagrange approach with the FW-H integral equation for the simulation of the mixed aerodynamic noise of solid particles, and the multiphase flow field and aerodynamic noise characteristics of the flow around a cylinder under windy and sandy conditions are studied. The aerodynamic force characteristics, flow dynamics, and noise characteristics of the single-phase and gas-solid two-phase flow around a cylinder are analyzed through a comparative study integrating theory of vortex dynamics. The mechanisms of interaction among particles, the vortex and noise are investigated, and the physical mechanisms of the flow and noise generation in the gas-solid flow around a cylinder are elucidated. The results indicate that, under the same inflow conditions, the time-averaged drag coefficient and surface pressure fluctuations on the cylinder of the gas-solid two-phase flow significantly increase compared to the single-phase flow field. A high-concentration area with a bow-shaped distribution of particles is observed on the upstream side of the cylinder, where small vortex structures appear. Moreover, the surface pressure fluctuations of the gas-solid two-phase flow increase, and the interaction area between the strong vorticity and the strong strain, represented by the Lamb vector divergence which is also the noise source term, increases. These two factors contribute to an increase in the flow field noise.

     

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