Theory of unsteady separation in supersonic flow around a convex corner

DOI10.1007/S10697-007-0052-4zbMath1354.76085OpenAlexW4245135459MaRDI QIDQ736071

R. Ya. Tugazakov

Publication date: 27 October 2009

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

Full work available at URL: https://doi.org/10.1007/s10697-007-0052-4

zbMATH Keywords

vortexshock waveunsteady flowinviscid gasflow around a cornerstall angle

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (2)

Hysteresis phenomenon in supersonic flow past a system of cylinders ⋮ On the theory of supersonic inviscid flow separation in gasdynamic problems

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