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Turbulent Inflow Generation for Direct Simulations of Hypersonic Turbulent Boundary Layers and their Freestream Acoustic Radiation

机译:直接模拟高超声速湍流边界层及其自由流声辐射的湍流产生

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Direct numerical simulations (DNS) of turbulent boundary layers and their freestream acoustic radiation are conducted with a recycling-rescaling based or a digital-filtering based turbulent inflow generation methodologies. The flow conditions of the simulations fall within the hypersonic regime where a systematic comparison of inflow methods has not been conducted before. The study provides a detailed comparison between the two distinct turbulent inflow generation methodologies at a common hypersonic condition, in terms of both the turbulence statistics within the boundary layer and the acoustic pressure statistics in the free stream. The study shows that simulation results compare well downstream of the inflow adjustment region between the recycling-rescaling and the digital-filtering based methodologies.
机译:湍流边界层及其自由流声辐射的直接数值模拟(DNS)使用基于再循环-缩放的或基于数字滤波的湍流产生方法进行。模拟的流动条件属于高超音速状态,在此之前尚未对流入方法进行过系统的比较。该研究就边界层内的湍流统计量和自由流中的声压统计量而言,在常见的高超声速条件下,提供了两种不同湍流产生方法之间的详细比较。研究表明,模拟结果在再循环调整和基于数字过滤的方法之间很好地比较了流入调节区域的下游。

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