| タイトル | Flow Field Around a Hovering Rotor |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970011616 |
| 著者（英） | Tung, C.; Low, S. |
| 著者所属（英） | Army Aviation Systems Command |
| 発行日 | 1997-02-01 |
| 言語 | eng |
| 内容記述 | A lifting surface hover code developed by the Analytical Method Inc. (AMI) was used to compute the average and unsteady velocity flow field of an isolated rotor without ground effect. The predicted velocity field compares well with experimental data obtained by hot-wire anemometry and by Laser Doppler Velocimetry. A subroutine 'DOWNWASH' was written to predict the velocity field at any given point in the wake for a given blade position. |
| NASA分類 | Aerodynamics |
| レポートNO | 97N16474
NASA-TM-110426
NAS 1.15:110426
A-975370
USAATCOM-TR-96-A-012 |
| 権利 | No Copyright |
