Breakdown of steady axisymmetric flow in the shock layer formed when a supersonic underexpanded jet interacts with a perpendicular flat plate

DOI10.1007/BF01051322zbMath0789.76056OpenAlexW2032273737MaRDI QIDQ1317738

E. I. Sokolov

Publication date: 12 April 1994

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

Full work available at URL: https://doi.org/10.1007/bf01051322

zbMATH Keywords

small perturbationsnonlinear formulationcentral shockself-oscillating unsteady regime

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

Cites Work

• Shock Fitting Method for Complicated Two-Dimensional Supersonic Flows

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