Large injection rates on unsteady compressible boundary layer flow over cones at angles of attack

DOI10.1007/BF00787533zbMath0828.76071OpenAlexW2093579349MaRDI QIDQ1896805

Yanyan Li

Publication date: 1995

Published in: Archive of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00787533

zbMATH Keywords

viscous dissipationimplicit schemequasi-linearization techniqueenthalpysymmetry planecross-flow parameter

Mathematics Subject Classification ID

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

Cites Work

• Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layer
• Nonsteady Three-Dimensional Stagnation Point Flow with Hard Blowing
• Fast and stable numerical method for boundary-layer flow with massive blowing
• Laminar flow at a three-dimensional stagnation point with large rates of injection
• Three-Dimensional Boundary Layer with Uniform Mass Transfer
• The solution of sharp-cone boundary-layer equations in the plane of symmetry

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