Supersonic flow past a wedge on a flat plate. Laminar boundary layer separation and reattachment

DOI10.1134/S0015462807060051zbMath1202.76082MaRDI QIDQ612495

A. D. Savel'ev

Publication date: 28 December 2010

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

zbMATH Keywords

Navier-Stokes equationsnumerical modelinglaminar boundary layer separationpressure at the reattachment pointseparation initiation criterion

Mathematics Subject Classification ID

Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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• Laminar boundary layer oblique shock wave interaction on flat and curved plates
• A Numerical Method for Solving the Equations of Compressible Viscous Flow
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations