Viscous flow over a cone at moderate incidence. I: Hypersonic tip region

DOI10.1016/0045-7930(73)90025-XzbMath0328.76052OpenAlexW1491433685MaRDI QIDQ1226928

T. C. Lin, Stanley G. Rubin

Publication date: 1973

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

Full work available at URL: https://doi.org/10.1016/0045-7930(73)90025-x

Mathematics Subject Classification ID

Finite difference methods for boundary value problems involving PDEs (65N06) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (11)

Global PNS solutions for subsonic strong interaction flow over a cone- cylinder-boattail configuration ⋮ Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layer ⋮ Non-Navier Stokes viscous flow computations ⋮ Pressure based flux-split solutions for incompressible and compressible internal flows ⋮ A computational procedure for supersonic flows governed by the parabolic Navier-Stokes equations ⋮ Viscous flow over a cone at moderate incidence. I: Hypersonic tip region ⋮ An implicit method for three dimensional viscous flow with application to cones at angle of attack ⋮ A review of strongly coupled algorithms for viscous flow problems ⋮ Viscous shock layer on a plate in hypersonic flow ⋮ A space-marching method for viscous incompressible internal flows ⋮ 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 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
• Hypersonic flows past a yawed circular cone and other pointed bodies
• Solution of a three-dimensional boundary-layer flow with separation.
• Hypersonic viscous flow over slender bodies with sharp leading edges.
• The hypersonic leading-edge problem.
• Theoretical and experimental study of rarefied supersonic flows about several simple shapes.
• On the two-dimensional viscous counterpart of the one-dimensional sonic throat
• Beam-continuum model for hypersonic flow over a flat plate.
• A predictor-corrector method for three coordinate viscous flows

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