Numerical analysis of supersonic viscous gas flow past axisymmetric blunt bodies

DOI10.1007/BF02698756zbMath0958.76037OpenAlexW1996581443MaRDI QIDQ1567873

N. Delaunay

Publication date: 9 April 2001

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf02698756

zbMATH Keywords

heat transferstabilization methodviscous shock layeraxisymmetric smooth blunt bodiesfinite one-sided backward differencessupersonic viscous homogeneous gas flow

Mathematics Subject Classification ID

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

Cites Work

• Computation of the viscous shock layer on blunted cones
• Numerical solution of the hypersonic viscous shock-layer equations
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Numerical analysis of supersonic viscous gas flow past axisymmetric blunt bodies