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• W3100293722 abstract "Above a critical angle, an oblique shock impinging on a Mach 5.92 boundary layer causes the resulting separated flow to become unstable. Direct numerical simulation and global stability analysis reveal the physical mechanism that drives this three-dimensional instability." @default.
• W3100293722 created "2020-11-23" @default.
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• W3100293722 date "2018-01-26" @default.
• W3100293722 modified "2023-10-16" @default.
• W3100293722 title "Simulation and stability analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92" @default.
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• W3100293722 doi "https://doi.org/10.1103/physrevfluids.3.013906" @default.
• W3100293722 hasPublicationYear "2018" @default.
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