On local recirculation zones in the supersonic boundary layer on a moving surface

DOI10.1016/0041-5553(82)90086-6zbMath0557.76040OpenAlexW2077937090MaRDI QIDQ3221605

V. I. Zhuk

Publication date: 1982

Published in: USSR Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0041-5553(82)90086-6

zbMATH Keywords

vorticityskin frictioninner flowouter flowplatefinite-difference schemestreamlinespressure distributionzoneunsteady separationstream and vorticity functionsweak shock wavecriterion of Moore-Rott-Searssupersonic boundary-layer on moving flat

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Supersonic flows (76J20)

Related Items (3)

Incompressible boundary layer with counterflows at a given pressure gradient ⋮ Singularity formation in an incompressible boundary layer on an upstream moving wall under given external pressure ⋮ On quasi-steady boundary-layer separation in supersonic flow. Part 2. Downstream moving separation point

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