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LES of a Transverse Jet into a Supersonic Crossflow

机译:将横向射流成超声波横向流量

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摘要

Numerical investigation of a transverse sonic jet injected into a supersonic crossflow was carried out using large-eddy simulation. Results have been validated carefully against experimental data. Turbulent behaviors relevant to the interaction of the jet and the supersonic crossflow are discussed. The complex flow structures and the relevant flow features are analyzed to exhibit the evolution of shock structures, vortical structures and jet shear layer.
机译:使用大涡模拟进行了注入超声波横向流入的横向声波喷射的数值研究。结果已经仔细验证了实验数据。讨论了与喷射器和超音速交叉流的相互作用相关的湍流行为。分析复杂的流动结构和相关的流动特征以表现出冲击结构,涡流结构和射流剪切层的演变。

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