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Turbulence Modelling and Meshing Developments for the Prediction of Jet Noise Installation Effects

机译:湍流建模和网格化开发,用于预测喷气噪声的安装效果

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Method developments targeting the efficient and accurate simulation of jet noise from complex, installed configurations are presented. Improvements to Detached-Eddy Simulation (DES) achieve a rapid development of resolved turbulence in the early shear layer region, which is of great importance for jet noise simulation. The practical non-zonal nature of DES is retained, while its efficient treatment of attached turbulent boundary layers enables the simulation of installation effects with feasible computational effort Alongside the turbulence modelling developments, a hybrid structured-unstructured meshing strategy is explored. This couples efficient anisotropic shear layer refinement in the structured jet plume region with practical unstructured meshing for the surrounding complex geometry. Although the need to ensure a smooth structured/unstructured transition leads to additional constraints, viable mitigation strategies have been proposed. Encouraging initial results for the near-field flow prediction and far-field sound prediction are presented and discussed.
机译:提出了针对复杂,已安装配置中的喷气噪声进行高效,准确模拟的方法开发。分离涡流仿真(DES)的改进实现了在早期剪切层区域快速解决湍流问题,这对于喷射噪声仿真非常重要。保留了DES的实用的非区域性,而对附着的湍流边界层的有效处理使得可以通过可行的计算工作来模拟安装效果。除了湍流建模的发展外,还探索了一种混合的结构化/非结构化网格划分策略。这将结构化射流羽流区域中有效的各向异性剪切层细化与周围复杂几何体的实际非结构化网格相结合。尽管需要确保平滑的结构化/非结构化过渡会导致其他约束,但已提出了可行的缓解策略。提出并讨论了令人鼓舞的近场流量预测和远场声音预测的初始结果。

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