Abstract
This report describes recent progress in the development and application of 3D Cartesian grid generation and Euler flow solution techniques. Improvements to flow field grid generation algorithms, geometry representations, and geometry refinement criteria are presented, including details of a procedure for correctly identifying and resolving extremely thin surface features. An initial implementation of automatic flow field refinement is also presented. Results for several 3D multi-component configurations are provided and discussed.
| Original language | English (US) |
|---|---|
| State | Published - Jan 1 1995 |
| Event | 33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995 |
Other
| Other | 33rd Aerospace Sciences Meeting and Exhibit, 1995 |
|---|---|
| Country | United States |
| City | Reno |
| Period | 1/9/95 → 1/12/95 |
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ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering
Cite this
Melton, J. E., Berger, M. J., Aftosmis, M. J., & Wong, M. D. (1995). 3D applications of a Cartesian grid Euler method. Paper presented at 33rd Aerospace Sciences Meeting and Exhibit, 1995, Reno, United States.