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BIBTEX RIS

Simulation and stability analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92

2018; American Physical Society; Volume: 3; Issue: 1 Linguagem: Inglês

10.1103/physrevfluids.3.013906

ISSN

2469-9918

Autores

Nathaniel Hildebrand, Anubhav Dwivedi, Joseph W. Nichols, Mihailo R. Jovanović, Graham V. Candler,

Tópico(s)

Gas Dynamics and Kinetic Theory

Resumo

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.

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