| タイトル | Measurements of the Early Development of Trailing Vorticity from a Rotor |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030003700 |
| 著者（英） | McAlister, Kenneth W.; Heineck, James T. |
| 著者所属（英） | Army Aviation and Missile Command|NASA Ames Research Center |
| 発行日 | 2002-07-01 |
| 言語 | eng |
| 内容記述 | The wake behind a two-bladed model rotor in light climb was measured using particle image velocimetry, with particular emphasis on the development of the trailing vortex during the first revolution of the rotor. The distribution of vorticity was distinguished from the slightly elliptical swirl pattern. Peculiar dynamics within the "void" region may explain why the peak vorticity appeared to shift away from the center as the vortex aged, suggesting the onset of instability. The swirl and axial velocities (which reached 44% and 12% of the rotor tip speed, respectively) were found to be asymmetric relative to the vortex center. In particular, the axial flow was composed of two concentrated zones moving in opposite directions. The radial distribution of the circulation rapidly increased in magnitude until reaching a point just beyond the core radius, after which the rate of growth decreased significantly. The core-radius circulation increased slightly with wake age, but the large-radius circulation appeared to remain relatively constant. The radial distributions of swirl velocity and vorticity exhibit self-similar behaviors, especially within the core. The diameter of the vortex core was initially about 10% of the rotor-blade chord, but more than doubled its size after one revolution of the rotor. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AFDD-TR-02-A-001
AD-A406980
NAS 1.60:211848
NASA/TP-2002-211848
A-0208212 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/90890 |
