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Simulation of transonic viscous wing and wing-fuselage flows using zonal methods
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Flores, Jolen |
| Copyright Year | 1987 |
| Description | The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition method) to develop the Transonic Navier-Stokes (TNS) wing-alone code. The TNS has a total of 4 zones and is extended to a total of 16 zones for the wing-fuselage version of the code. Results are compared on the Cray X-MP-48 and compared with experimental data. |
| File Size | 2714279 |
| Page Count | 69 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870010809 |
| Archival Resource Key | ark:/13960/t7kq2wn5p |
| Language | English |
| Publisher Date | 1987-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Transonic Flow Algorithms Three Dimensional Flow Body-wing Configurations Computational Fluid Dynamics Flow Distribution Computational Grids Cray Computers Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
