Efficient numerical method for simulation of supersonic viscous flow past a blunted body at a small angle of attack

DOI10.1016/0045-7930(94)90029-9zbMath0782.76068OpenAlexW2164587086MaRDI QIDQ1309609

G. A. Tirskij, Sergey V. Utyuzhnikov, Nail K. Yamaleev

Publication date: 24 February 1994

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

Full work available at URL: https://doi.org/10.1016/0045-7930(94)90029-9

zbMATH Keywords

asymptotic methodshock wavepressure gradientsmall parameter methodfull viscous shock-layer equationsmethod of global iterationsone- parameter family of solutions

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (4)

Numerical simulation of the flow over a body flying through a thermal in a stratified atmosphere ⋮ Dispersive and dissipative properties of the fully discrete bicompact schemes of the fourth order of spatial approximation for hyperbolic equations ⋮ Some new approaches to building and implementation of wall-functions for modeling of near-wall turbulent flows ⋮ Spatial supersonic motion of a body through a large-scale inhomogeneity in a stratified atmosphere

Cites Work

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• Grid adaption for problems in fluid dynamics
• Three-Dimensional Supersonic Viscous Flow over a Cone at Incidence
• Numerical solution of the hypersonic viscous shock-layer equations
• On Supersonic Flow Past A Slightly Yawing Cone

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