Three-dimensional steady supersonic duct flow using Lagrangian formulation

DOI10.1007/BF01414718zbMath0790.76056MaRDI QIDQ1317347

Meng-Sing Liou, Ching Y. Loh

Publication date: 5 July 1994

Published in: Shock Waves (Search for Journal in Brave)

zbMATH Keywords

Euler equationswave interactionscontact discontinuitiesTVD schemestreamwise marching Lagrangian method

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (2)

Kolmogorov n-width and Lagrangian physics-informed neural networks: a causality-conforming manifold for convection-dominated PDEs ⋮ A free-Lagrange method for unsteady compressible flow: Simulation of a confined cylindrical blast wave

Cites Work

• A new Lagrangian method for steady supersonic flow computation. I: Godunov scheme
• Numerical solutions for supersonic corner flow
• Towards the ultimate conservative difference scheme. IV: A new approach to numerical convection

This page was built for publication: Three-dimensional steady supersonic duct flow using Lagrangian formulation