Hypersonic transition induced by three isolated roughness elements on a flat plate

DOI10.1016/J.COMPFLUID.2017.08.006zbMath1390.76278OpenAlexW2742615505MaRDI QIDQ1648518

Zhixiang Xiao, Zhiwei Duan

Publication date: 27 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2017.08.006

zbMATH Keywords

boundary layerhypersonicroughness induced transition

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Hypersonic flows (76K05) Transition to turbulence (76F06)

Related Items (2)

Direct numerical simulation of high-speed transition due to roughness elements ⋮ First-mode-induced nonlinear breakdown in a hypersonic boundary layer

Cites Work

• A class of finite difference schemes with low dispersion and controllable dissipation for DNS of compressible turbulence
• Laminar–turbulent transition induced by a discrete roughness element in a supersonic boundary layer
• High-speed boundary-layer transition induced by a discrete roughness element
• Unnamed Item

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