Boundary layer dynamics in a compressible gas. Numerical simulation

DOI10.1134/S0015462822020148zbMath1501.76069OpenAlexW4220758563MaRDI QIDQ2086800

V. A. Zharov, R. Ya. Tugazakov

Publication date: 26 October 2022

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

Full work available at URL: https://doi.org/10.1134/s0015462822020148

zbMATH Keywords

Navier-Stokes equationssupersonic flowspectral analysislaminar-turbulent transitiontwo-step difference schemeturbulent spotresonant three-wave wave amplification

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Turbulent boundary layers (76F40) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Transition to turbulence (76F06) Compressible Navier-Stokes equations (76N06)

Uses Software

• Mathematica

Cites Work

• Generation of coherent structures in supersonic flow past a finite-span flat plate
• On the theory of supersonic inviscid flow separation in gasdynamic problems
• Late-stage transitional boundary-layer structures. Direct numerical simulation and experiment
• Optimal axisymmetric noses of bodies in a flow. Calculations and experiments
• Three-dimensional turbulent supersonic flow over a plate
• Difference for the inviscid and viscous equations of a compressible gas
• Tollmien-Schlichting-wave resonant mechanism for subharmonic-type transition
• The structure of turbulent boundary layers
• Non-linear resonant instability in boundary layers

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