| タイトル | Study of vortex breakdown of F-106B by Euler code |
| 著者（英） | Pao, Jenn Louh |
| 著者所属（英） | Vigyan Research Associates, Inc. |
| 発行日 | 1990-02-01 |
| 言語 | eng |
| 内容記述 | The 'Three-dimensional Euler Aerodynamic Method' (TEAM) is presently applied to the F-106B at subsonic speed, in order to examine the relationship between off- and on-surface flow features at angles-of-attack sufficiently great for the occurrence of vortex breakdown. Although TEAM's flow separation is triggered by numerical dissipation, the general trend of vortex-breakdown effect on computed lift characteristics is similar to extant wind tunnel results. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 90A23289 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/358243 |
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