A computational procedure for supersonic flows governed by the parabolic Navier-Stokes equations

DOI10.1016/0021-9991(80)90075-3zbMath0453.76063OpenAlexW2028734444MaRDI QIDQ1149336

S. H. Smith

Publication date: 1980

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

Full work available at URL: https://doi.org/10.1016/0021-9991(80)90075-3

zbMATH Keywords

method of fractional stepstwo-dimensionalfinite width platemultidimensional difference operatornonuniform mesh systems

Mathematics Subject Classification ID

Numerical computation of solutions to systems of equations (65H10) Finite difference methods applied to problems in fluid mechanics (76M20) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Stability and convergence of numerical methods for initial value and initial-boundary value problems involving PDEs (65M12) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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• Numerical method for predicting three-dimensional steady viscous flow in ducts
• 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
• Solution of the multidimensional compressible Navier-Stokes equations by a generalized implicit method
• An alternating directional implicit scheme for three-dimensional hypersonic flows
• A numerical method for three-dimensional viscous flow: Application to the hypersonic leading edge
• A calculation procedure for heat, mass and momentum transfer in three- dimensional parabolic flows

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