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Noise Prediction of the LAGOON Landing Gear Using Detached Eddy Simulation and Acoustic Analogy

机译:基于分离涡模拟和声学模拟的LAGOON起落架噪声预测

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This paper presents detached eddy simulations, DES, of the LAGOON landing gear configuration performed using different unstructured meshes. We employ the BCFD code for the DES calculations and results are compared to experimental measurements available in the literature. An implicit dual-time stepping method is employed together with an optimized second-order backward-differencing scheme. For the spatial discretization, a second order accurate HLLE scheme is employed together with a bounded central differencing approach to reduce numerical dissipation of the flux reconstruction. Results are presented in terms of steady and unsteady hydrodynamic data as well as noise predictions, which are performed using the Ffowcs Williams & Hawkings formulation. Overall, numerical results show a good agreement with experimental data. The paper also includes an assessment of the proper orthogonal decomposition, POD, of the unsteady flow field in order to identify coherent energetic structures responsible for the cavity tonal noise mechanism at specific frequencies. Here, the POD technique employs a filter function to the correlation matrix which allows the analysis of POD spatial eigenmodes at specific frequencies. At 1.5 kHz, coherent structures which are responsible for tonal noise generation are observed along the cavity. Results from a wavelet decomposition demonstrate that the sound generation in the cavity is an intermittent process.
机译:本文介绍了使用不同的非结构化网格对LAGOON起落架构型进行的分离涡流仿真DES。我们使用BCFD代码进行DES计算,并将结果与​​文献中提供的实验测量结果进行比较。隐式双时间步进方法与优化的二阶后向差分方案一起使用。对于空间离散化,采用二阶准确的HLLE方案以及有界的中心差分方法来减少通量重构的数值耗散。结果以稳态和非稳态流体力学数据以及噪声预测的形式表示,这些数据是使用Ffowcs Williams&Hawkings公式执行的。总体而言,数值结果表明与实验数据吻合良好。该论文还包括对非恒定流场的适当正交分解POD的评估,以识别在特定频率下引起腔音调噪声机制的相干高能结构。在此,POD技术对相关矩阵采用了滤波函数,从而可以分析特定频率下的POD空间本征模。在1.5 kHz处,沿空腔观察到产生音调噪声的相干结构。小波分解的结果表明,空腔中的声音生成是一个间歇过程。

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