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Multidomain approach for calculating compressible flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chazzi, W. Veuillot, J. P. Viviand, H. Cambier, L. |
| Copyright Year | 1982 |
| Description | A multidomain approach for calculating compressible flows by using unsteady or pseudo-unsteady methods is presented. This approach is based on a general technique of connecting together two domains in which hyperbolic systems (that may differ) are solved with the aid of compatibility relations associated with these systems. Some examples of this approach's application to calculating transonic flows in ideal fluids are shown, particularly the adjustment of shock waves. The approach is then applied to treating a shock/boundary layer interaction problem in a transonic channel. |
| File Size | 1612125 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820022410 |
| Archival Resource Key | ark:/13960/t6353gh2q |
| Language | English |
| Publisher Date | 1982-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Shock Waves Transonic Flow Turbulent Flow Computational Fluid Dynamics Ideal Fluids Shock Wave Interaction Unsteady Flow Channel Flow Compressible Flow Boundary Layers Hyperbolic Differential Equations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
