| タイトル | Drag reduction on a bluff body at yaw angles to 30 degrees |
| 著者（英） | Goodman, Wesley L.; Howard, Floyd G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-04-01 |
| 言語 | eng |
| 内容記述 | The base separation alleviation and drag reduction effectiveness of transverse rectangular grooves and longitudinal v-grooves in the afterbody shoulder region of a bluff body is investigated for body yaw angles of 0-30 deg. The grooves are found to be beneficial in reducing both freestream and axial drag coefficients at yaw angles of up to 25 deg. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 87A34465 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/378466 |
