Vortex structures evolution in supersonic mixing layers with different inlet Reynolds numbers based on the Lagrangian method

The supersonic mixing layer is a typical flow structure in an aircraft’s optical seeker. The free incoming flow and cooling jet form a mixing layer through shearing. In most cases, the flow has become a fully developed turbulent due to complex factors during flight. This paper mainly focuses on the...

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Veröffentlicht in:AIP advances 2021-12, Vol.11 (12), p.125128-125128-12
Hauptverfasser: Xing, Boyang, Li, Dongdong, Zhang, Bin, Xu, Hui, Liu, Hong
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Sprache:eng
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