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Moving and adaptive grid methods for compressible flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Camarero, Ricardo Trepanier Sr., Jean-Yves |
| Copyright Year | 1995 |
| Description | This paper describes adaptive grid methods developed specifically for compressible flow computations. The basic flow solver is a finite-volume implementation of Roe's flux difference splitting scheme or arbitrarily moving unstructured triangular meshes. The grid adaptation is performed according to geometric and flow requirements. Some results are included to illustrate the potential of the methodology. |
| File Size | 5395591 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19960011641 |
| Archival Resource Key | ark:/13960/t4fn63n4f |
| Language | English |
| Publisher Date | 1995-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Shock Waves Boundary Value Problems Algorithms Computational Fluid Dynamics Unstructured Grids Mathematics Two Dimensional Models Finite Volume Method Unsteady Flow Grid Generation Mathematics Wedges Compressible Flow Flux Difference Splitting Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |