Abstract
The multiple one-dimensional adaptive grid procedure is modified by several methods of smoothing the weighting function. A two-dimensional oblique shock reflection problem is employed to demonstrated details and effects of the proposed adaptive grid method. Numerical examination exhibits that all the smoothing methods improve’ the original method effectively. Finally, a strategy to combine these smoothing techniques is proposed.
| Original language | English |
|---|---|
| DOIs | |
| Publication status | Published - 1999 |
| Event | 37th Aerospace Sciences Meeting and Exhibit, 1999 - Reno, United States Duration: 1999 Jan 11 → 1999 Jan 14 |
Other
| Other | 37th Aerospace Sciences Meeting and Exhibit, 1999 |
|---|---|
| Country/Territory | United States |
| City | Reno |
| Period | 99-01-11 → 99-01-14 |
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering