| タイトル | Unsteady Validation of a Mean Flow Boundary Condition for Computational Aeroacoustics |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050207428 |
| 著者（英） | Sawyer, S>; Nallasamy, M.; Hixon, R.; Dyson, R.; Zhen, F. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2004-01-01 |
| 言語 | eng |
| 内容記述 | In this work, a previously developed mean flow boundary condition will be validated for unsteady flows. The test cases will be several reference benchmark flows consisting of vortical gusts convecting in a uniform mean flow, as well as the more realistic case of a vortical gust impinging on a loaded 2D cascade. The results will verify that the mean flow boundary condition both imposes the desired mean flow as well as having little or no effect on the instantaneous unsteady solution. |
| NASA分類 | Acoustics |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/219629 |
