Modeling of supersonic/hypersonic boundary layer transition using a single-point approach

DOI10.1515/ijnsns-2017-0011zbMath1401.76117OpenAlexW2796164835MaRDI QIDQ1662877

Y. Aharonov

Publication date: 20 August 2018

Published in: International Journal of Nonlinear Sciences and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1515/ijnsns-2017-0011

zbMATH Keywords

intermittencyboundary layer transitionlaminar fluctuationssupersonic/ hypersonic flows

Mathematics Subject Classification ID

Supersonic flows (76J20) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• A Favré averaged transition prediction model for hypersonic flows
• Development of an intermittency equation for the modeling of the supersonic/hypersonic boundary layer flow transition
• Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
• Computation of hypersonic double wedge shock / boundary layer interaction
• Transition in Wall-Bounded Flows
• The stabilizing effect of compressibility in turbulent shear flow
• Transition model for high-speed flow
• The analysis and modelling of dilatational terms in compressible turbulence

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