| タイトル | Wind-tunnel tests and computer simulations of buoyant wing-tip vortices |
| 著者（英） | Costen, R. C.; Rogers, G. T.; Davidson, R. E. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | It is demonstrated that wing-tip vortices with buoyant cores can be made in a wind tunnel. Wing-tip vortices generated by an aircraft often become buoyant, because of heating effects due to the jet exhaust or in connection with a descending motion in a stable atmosphere. A description of wind-tunnel studies is given, taking into account the experimental conditions, the transition to turbulence, and the drift of the buoyant vortex. A computer simulation of wing-tip vortices is also discussed. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 75A35422 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/447681 |
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