Mach wave effect on laminar-turbulent transition in supersonic flow over a flat plate

DOI10.1134/S0015462818050063zbMath1407.76039OpenAlexW2907023464WikidataQ128692330 ScholiaQ128692330MaRDI QIDQ1728748

Xianqiang Yang

Publication date: 25 February 2019

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462818050063

zbMATH Keywords

supersonic flowboundary layerTollmien-Schlichting wavenumerical modelingMach wavequasistationary wake

Mathematics Subject Classification ID

Supersonic flows (76J20) Transition to turbulence (76F06)

Related Items (2)

Numerical simulation of the interaction of unsteady surface blowing (suction) with turbulent near-wall flow ⋮ Prediction of laminar-turbulent transition on flat plate on the basis of stochastic theory of turbulence and equivalence of measures

Cites Work

• Direct numerical simulation of laminar-turbulent flow over a flat plate at hypersonic flow speeds
• Efficient implementation of weighted ENO schemes
• Unnamed Item

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