A numerical method for three-dimensional viscous flow: Application to the hypersonic leading edge

DOI10.1016/0021-9991(72)90027-7zbMath0243.76040OpenAlexW2016314391MaRDI QIDQ2554638

Stanley G. Rubin, T. C. Lin

Publication date: 1972

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-9991(72)90027-7

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items

Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layer ⋮ A computational procedure for supersonic flows governed by the parabolic Navier-Stokes equations ⋮ Compressible corner flow ⋮ 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 ⋮ Viscous flow solutions with a cubic spline approximation ⋮ Three-dimensional supersonic flow of a viscous or inviscid gas ⋮ A review of strongly coupled algorithms for viscous flow problems ⋮ Polynomial interpolation methods for viscous flow calculations ⋮ Turbulent modeling of a vortex boundary layer flow ⋮ Laminar flow in rectangular channels. Part I: entry analysis. Part II: numerical solution for a square channel ⋮ On the outflow conditions for spectral solution of the viscous blunt-body problem ⋮ Numerical solution of Navier-Stokes equations for viscous gas by the semimarching method

Cites Work

• Unnamed Item
• The Numerical Solution of Parabolic and Elliptic Differential Equations
• Hypersonic viscous flow over slender bodies with sharp leading edges.