| タイトル | Flow-field Survey of an Empennage Wake Interacting with a Pusher Propeller |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890002323 |
| 著者（英） | Soderman, Paul T.; Horne, W. Clifton |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1988-10-01 |
| 言語 | eng |
| 内容記述 | The flow field between a model empennage and a 591-mm-diameter pusher propeller was studied in the Ames 7- by 10-Foot Wind Tunnel with directional pressure probes and hot-wire anemometers. The region probed was bounded by the empennage trailing edge and downstream propeller. The wake properties, including effects of propeller operation on the empennage wake, were investigated for two empennage geometries: one, a vertical tail fin, the other, a Y-tail with a 34 deg dihedral. Results showed that the effect of the propeller on the empennage wake upstream of the propeller was not strong. The flow upstream of the propeller was accelerated in the streamwise direction by the propeller, but the empennage wake width and velocity defect were relatively unaffected by the presence of the propeller. The peak turbulence in the wake near the propeller tip station, 0.66 diameter behind the vertical tail fin, was approximately 3 percent of the free-stream velocity. The velocity field data can be used in predictions of the acoustic field due to propeller-wake interaction. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 89N11694
A-88185
NAS 1.15:101003
NASA-TM-101003 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/65594 |
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