| タイトル | Preliminary study of a wing-tip vortex using laser velocimetry |
| 本文(外部サイト) | http://hdl.handle.net/2060/19870005752 |
| 著者(英) | Takahashi, R. K.; Mcalister, K. W. |
| 著者所属(英) | NASA Ames Research Center |
| 発行日 | 1987-01-01 |
| 言語 | eng |
| 内容記述 | Measurements have been made in the wake of a semi-span NACA 0015 airfoil with emphasis on the region of the wing tip vortex. The spanwise and streamwise velocity components were measured using a two-component laser Doppler velocimeter. The purpose of the study was to initiate the operation of a laser velocimeter system and to perform preliminary wake measurements in preparation for a more extensive study of the structure and near field development of a tip vortex. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 87N15185 AVSCOM-TM-86-A-2 NASA-TM-88343 NAS 1.15:88343 A-86207 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/152567 |