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Large-eddy simulation of supersonic turbulent flow in axisymmetric nozzles and diffusers

机译:轴对称喷嘴和扩压器中超音速湍流的大涡模拟

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摘要

Effects of extra strain and dilatation rates on the turbulence structure in nozzles and diffusers with fully developed supersonic pipe flow as inflow condition are investigated by means of LES using high-order numerical schemes. Results from a DNS of pipe and nozzle flow validating the LES are also shown. It is found that weak pressure gradients already strongly inhibit or enhance the Reynolds stresses via corresponding changes of production and pressure-strain terms. The results constitute a database for the improvement of second-order turbulence models for compressible flow.
机译:利用高阶数值方案,利用LES研究了超音速管流完全发展为流入条件的喷嘴和扩压器湍流结构的额外应变和膨胀率的影响。还显示了通过管道和喷嘴流量的DNS验证LES的结果。发现弱的压力梯度已经通过生产和压力-应变项的相应变化强烈地抑制或增强了雷诺应力。结果构成用于改进可压缩流的二阶湍流模型的数据库。

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