Three-dimensional steady supersonic duct flow using Lagrangian formulation (Q1317347)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Three-dimensional steady supersonic duct flow using Lagrangian formulation |
scientific article; zbMATH DE number 528955
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Three-dimensional steady supersonic duct flow using Lagrangian formulation |
scientific article; zbMATH DE number 528955 |
Statements
Three-dimensional steady supersonic duct flow using Lagrangian formulation (English)
0 references
5 July 1994
0 references
A numerical simulation of three-dimensional supersonic flow in a duct is presented. The flow field in the duct is complex and can find its applications in the inlet of air-breathing engines. A unique streamwise marching Lagrangian method is employed for solving the steady Euler equations. The new scheme is shown to be capable of accurately resolving complicated shock or contact discontinuities and their interactions. In all the computations, a free stream of Mach number \(M=4\) is considered.
0 references
TVD scheme
0 references
wave interactions
0 references
streamwise marching Lagrangian method
0 references
Euler equations
0 references
contact discontinuities
0 references
