| タイトル | Turbulent Output-Based Anisotropic Adaptation |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100002812 |
| 著者（英） | Carlson, Jan-Renee; Park, Michael A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2010-01-04 |
| 言語 | eng |
| 内容記述 | Controlling discretization error is a remaining challenge for computational fluid dynamics simulation. Grid adaptation is applied to reduce estimated discretization error in drag or pressure integral output functions. To enable application to high O(10(exp 7)) Reynolds number turbulent flows, a hybrid approach is utilized that freezes the near-wall boundary layer grids and adapts the grid away from the no slip boundaries. The hybrid approach is not applicable to problems with under resolved initial boundary layer grids, but is a powerful technique for problems with important off-body anisotropic features. Supersonic nozzle plume, turbulent flat plate, and shock-boundary layer interaction examples are presented with comparisons to experimental measurements of pressure and velocity. Adapted grids are produced that resolve off-body features in locations that are not known a priori. |
| NASA分類 | Aerodynamics |
| レポートNO | AIAA Paper 2010-168
LF99-8920 |
| 権利 | No Copyright |
