| タイトル | Performance and loads data from an outdoor hover test of a Lynx tail rotor |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890016587 |
| 著者（英） | Smith, Charles A.; Hagen, Martin J.; Signor, David B.; Yamauchi, Gloria K. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1989-06-01 |
| 言語 | eng |
| 内容記述 | A Lynx tail rotor was tested in hover at the Outdoor Aerodynamic Research Facility at NASA Ames Research Center. The test objectives were to measure the isolated rotor performance to provide a baseline for subsequent testing, and to operate the rotor throughout the speed and collective envelope before testing in the NFAC 40- by 80-Foot Wind Tunnel. Rotor forces and blade bending moments were measured at ambient wind conditions from zero to 6.23 m/sec. The test envelope was limited to rotor speeds of 1550 to 1850 rpm and minus 13 deg to plus 20 deg of blade collective pitch. The isolated rotor performance and blade loads data are presented. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 89N25958
A-89014
NASA-TM-101057
NAS 1.15:101057 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/141400 |
