High-Order Upwind Multi-Layer Compact Scheme (MLC) With Shock-Fitting Method for Two-Dimensional Supersonic Flows
AIAA AVIATION FORUM AND ASCEND 2024
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A cell-vertex upwind scheme for two-dimensional supersonic Euler flows
Online Contents | 1997
|Upwind Unstructured Scheme for Three-Dimensional Combusting Flows
Online Contents | 1996
|