Plate-injection into a separated supersonic boundary layer. Part 2. The transition regions

DOI10.1017/S0022112074000693zbMath0273.76051MaRDI QIDQ5181015

Keith Stewartson

Publication date: 1974

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

Mathematics Subject Classification ID

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

Related Items (2)

Injection from a finite section of a flat plate placed parallel to a uniform stream ⋮ Removal of Goldstein's singularity at separation, in flow past obstacles in wall layers

Cites Work

• The Navier-Stokes solution for laminar flow past a semi-infinite flat plate
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

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