Nonuniform slot injection (suction) into a compressible flow.

DOI10.1007/BF01170181zbMath1064.76093OpenAlexW2069308752MaRDI QIDQ1570849

S. Roy

Publication date: 2000

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01170181

zbMATH Keywords

separation pointcompressible boundary layerquasilinear implicit finite difference scheme

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (3)

Radiation effect on the turbulent compressible boundary layer flow with adverse pressure gradient ⋮ Methods of optimizing separation of compressible turbulent boundary-layer over a wedge with heat and mass transfer ⋮ MHD compressible turbulent boundary-layer flow with adverse pressure gradient

Cites Work

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• On strong slot injection into a subsonic laminar boundary layer
• Non-uniform slot injection into a laminar boundary layer
• Non-uniform slot injection (suction) or wall enthalpy into a steady nonsimilar compressible laminar boundary layer
• Numerical Study of Strong Slot Injection into a Supersonic Laminar Boundary Layer
• Three-dimensional laminar boundary layers and the ok of accessibility
• Finite-Difference Version of Quasi-Linearization Applied to Boundary-Layer Equations
• On solutions of the compressible laminar boundary-layer equations and their behaviour near separation
• Supersonic Laminar Boundary-Layer Separation by Slot Injection
• Comment on "Controllability Limit of a Human Pilot"
• On slot injection into a supersonic laminar boundary layer
• SOLUTION OF THE INCOMPRESSIBLE LAMINAR BOUNDARY-LAYER EQUATIONS

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