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Automatic computation of euler-marching and subsonic grids for wing-fuselage configurations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Adams, Mary S. Barger, Raymond L. Krishnan, Ramki R. |
| Copyright Year | 1994 |
| Description | Algebraic procedures are described for the automatic generation of structured, single-block flow computation grids for relatively simple configurations (wing, fuselage, and fin). For supersonic flows, a quasi two-dimensional grid for Euler-marching codes is developed, and some sample results in graphical form are included. A type of grid for subsonic flow calculation is also described. The techniques are algebraic and are based on a generalization of the method of transfinite interpolation. |
| File Size | 1139011 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940032443 |
| Archival Resource Key | ark:/13960/t01023f5b |
| Language | English |
| Publisher Date | 1994-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Body-wing Configurations Computational Fluid Dynamics Subsonic Flow Fins Fuselages Computational Grids Grid Generation Mathematics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
