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Large-eddy simulation of underexpanded sonic coaxial jet

机译:Underexpanded Sonic Coaxial Jet的大涡模拟

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Numerical investigation of underexpanded sonic coaxial jets was carried out using large-eddy simulation. The system consists of two coaxial nozzles, in which one is inner round nozzle and another is outer annular nozzle. Since the pressure ratio of inner to outer nozzle dominates the flow structures and behaviors, two typical pressure ratios 5/3 (case A) and 3/5 (case B) are considered. The calculated results have been validated carefully against experimental data. Based on the analysis of the flow structures, different shock systems and vortex shedding processes for the two cases are identified and some main flow characteristics of sonic coaxial jets are found. The power spectral analysis of pressure evolution is performed to demonstrate the frequency characters in the flow field. The mixing behaviors determined by different approaches are also discussed. The results obtained in this study provide physical insight into the understanding of the mechanisms relevant to the underexpanded sonic coaxial jets interaction.
机译:利用大涡模拟进行了Underexpanded Sonic同轴喷射的数值研究。该系统由两个同轴喷嘴组成,其中一个是内圆形喷嘴,另一个是外环形喷嘴。由于内部到外喷嘴的压力比主要地定位流动结构和行为,因此考虑两个典型的压力比(壳体A)和3/5(CASE B)。计算结果已经仔细验证了实验数据。基于对流动结构的分析,鉴定了两种情况的不同冲击系统和涡旋脱落过程,并发现了声波同轴喷射器的一些主要流动特性。执行压力演进的功率谱分析以展示流场中的频率字符。还讨论了不同方法确定的混合行为。本研究中获得的结果提供了物理洞察,以了解与Unterexpanced Sonic同轴喷射相互作用相关的机制。

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