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Gas injection and suction effect on the instability of a supersonic boundary layer

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Publication:6114741
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DOI10.1134/S001546282260184XzbMath1528.76029OpenAlexW4376880756MaRDI QIDQ6114741

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Publication date: 12 July 2023

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

Full work available at URL: https://doi.org/10.1134/s001546282260184x


zbMATH Keywords

Navier-Stokes equationsflat plate flowlinear stability theory\(e^N\) methodimplicit shock-capturing finite volume method


Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Parallel shear flows in hydrodynamic stability (76E05) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Compressible Navier-Stokes equations (76N06)





Cites Work

  • On the inviscid acoustic-mode instability of supersonic shear flows. I: Two-dimensional waves
  • Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer




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