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Automation of a n-s s and c database generation for the harrier in ground effect
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Murman, Scott M. Pandya, Shishir Chaderjian, Neal M. |
| Copyright Year | 2001 |
| Description | A method of automating the generation of a time-dependent, Navier-Stokes static stability and control database for the Harrier aircraft in ground effect is outlined. Reusable, lightweight components arc described which allow different facets of the computational fluid dynamic simulation process to utilize a consistent interface to a remote database. These components also allow changes and customizations to easily be facilitated into the solution process to enhance performance, without relying upon third-party support. An analysis of the multi-level parallel solver OVERFLOW-MLP is presented, and the results indicate that it is feasible to utilize large numbers of processors (= 100) even with a grid system with relatively small number of cells (= 10(exp 6)). A more detailed discussion of the simulation process, as well as refined data for the scaling of the OVERFLOW-MLP flow solver will be included in the full paper. |
| File Size | 1090998 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020022031 |
| Archival Resource Key | ark:/13960/t7dr7sw8q |
| Language | English |
| Publisher Date | 2001-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Navier-stokes Equation Computational Fluid Dynamics Static Stability Flow Distribution Automatic Control Harrier Aircraft Computerized Simulation Ground Effect Aerodynamics Grid Generation Mathematics Data Bases Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
