Evolution of artificial perturbations in the boundary layer on a plate and in its wake at supersonic free-stream velocity

DOI10.1023/A:1020689219093zbMath1161.76335OpenAlexW18129616MaRDI QIDQ1403620

V. I. Lysenko, Yu. G. Ermolaev

Publication date: 3 September 2003

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

Full work available at URL: https://doi.org/10.1023/a:1020689219093

zbMATH Keywords

supersonic flowboundary layerplatewakerarefaction wavesbackward-facing wedge

Mathematics Subject Classification ID

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

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