Laminar boundary-layer reattachment in supersonic flow. Part 2. Numerical solution

DOI10.1017/S0022112080002467zbMath0431.76034MaRDI QIDQ3868970

P. G. Daniels

Publication date: 1980

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

supersonic flownumerical solutiontriple-deck structurelaminar boundary-layer reattachment

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10)

Related Items (1)

Asymptotic model of a closed separation zone in supersonic flow

Cites Work

• The interaction of a shock wave with a laminar boundary layer

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