横掠二维串列双圆柱绕流气动噪声的数值模拟
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重庆市自然科学基金资助项目(CSTC2007BB6184);中国博士后科学基金资助项目(20080460753)


Aeroacoustics numerical simulation of flow past towdimensional two circular cylinders in Tandem arrangements
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    摘要:

    对横掠串列双圆柱绕流噪声问题进行数值模拟,首先通过二维大涡模拟(LES)求解非定常不可压缩NS方程捕获瞬时流场声源数据;然后运用基于Lighthill’s 声学类比的FWH方程及其积分解,计算由流体流动诱发产生的噪声。通过比较不同流速、直径、间距比对绕流流场以及由其产生的气动噪声的影响发现:流速、直径增加,辐射噪声级相应增大;流速增加,旋涡脱落频率增大;不同间距比对圆柱旋涡脱落有一定影响,从而影响到辐射噪声,存在噪声最大的临界间距比;同时辐射声场具有较明显的指向性。

    Abstract:

    The flow mechanism of flowing over two circular cylinders in tandem arrangements is numerically investigated. First, the unsteady incompressible NavierStokes equation is solved using twodimensional large eddy simulation (LES) model in order to capture the flow instantaneous source data. Then both the FWH equation and its integral solutions based on Lighthill’s acoustic analogy are employed to compute the noise generated by fluid flow. Different flow velocity, circle cylinder diameter and spacing ratios are compared. The result shows that the SPL augments with the increase of flow velocity or circle cylinder diameter. The frequency of vortices shedding is raised with the increase of flow velocity. Different spacing ratios impact the vortices shedding at a certain extent, and as a result impact the acoustic noise. There is the largest SPL near the critical spacing and the direction of acoustic fields is obvious.

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赵良举,杨南奇,吴朵,苏成功.横掠二维串列双圆柱绕流气动噪声的数值模拟[J].重庆大学学报,2009,32(8):943-949.

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