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Hybrid Finite Volume and Discontinuous Galerkin Method with Dynamic Overset Noise Source Identification for Acoustics Prediction

机译:动态超限噪声源识别的混合有限体积和间断Galerkin方法进行声学预测

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A novel approach for the accurate modeling of acoustic signal propagation is presented. In this work, a well-established unstructured mesh CFD solver is utilized to efficiently model the physics associated with acoustics generation and a high-order accurate discontinuous Galerkin solver is then used to accurately propagate acoustic signals across large distances with minimal dissipation and dispersion. The two solvers operate on separate overlapping meshes and an innovative dynamic overset coupling approach is used to transmit the acoustic signals to the farfield in a one-way manner in which the acoustics prediction is unaffected by the outer acoustic propagation physics. The acoustic source region is identified on-the-fly by means of a specialized dynamic hole-cutting and overset grid assembly approach based on proximity to regions of high pressure variance or Lighthill's stress. The framework upon which the solvers are developed is described along with details outlining the dynamic overset grid assembly and interpolation methods. Detailed parametric studies are conducted to demonstrate dynamic acoustic source identification using both statistical and instantaneous flow properties, and results are presented which verify the accuracy of the capability for aeroacoustic predictions.
机译:提出了一种新颖的方法,用于对声信号传播进行精确建模。在这项工作中,使用完善的非结构化网格CFD解算器来有效地建模与声学生成相关的物理过程,然后使用高阶准确的不连续Galerkin解算器来准确地传播声信号,并以最小的耗散和色散实现大范围的传播。这两个求解器在单独的重叠网格上运行,并且采用了创新的动态过载耦合方法,将声信号以单向方式传输到远场,在这种方式中,声波预测不受外部声波传播物理学的影响。声源区域可以根据靠近高压变化或Lighthill应力的区域的位置,通过专门的动态孔切割和冲孔网格装配方法即时识别。描述了开发求解器所基于的框架,并概述了概述动态过冲网格装配和插值方法的详细信息。进行了详细的参数研究,以证明使用统计流量和瞬时流量特性进行动态声源识别,并给出了验证航空声学预测能力准确性的结果。

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