An implicit method for three dimensional viscous flow with application to cones at angle of attack

DOI10.1016/0045-7930(75)90010-9zbMath0329.76069OpenAlexW2008676229MaRDI QIDQ1227349

Stephen C. Lubard, William S. Helliwell

Publication date: 1975

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(75)90010-9

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20) Numerical solution of discretized equations for boundary value problems involving PDEs (65N22)

Related Items (2)

A computational procedure for supersonic flows governed by the parabolic Navier-Stokes equations ⋮ Numerical solution of Navier-Stokes equations for viscous gas by the semimarching method

Cites Work

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• Viscous flow over a cone at moderate incidence. I: Hypersonic tip region
• A general formulation of alternating direction methods. I: Parabolic and hyperbolic problems
• A numerical method for three-dimensional viscous flow: Application to the hypersonic leading edge
• Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layer
• Calculation of the Flow on a Cone at High Angle of Attack
• Integration of Stiff Equations

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