| タイトル | Development of a Free-to-Roll Transonic Test Capability (Invited) |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030013633 |
| 著者（英） | Hall, R. M.; Owens, D. B.; Capone, F. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2003-01-01 |
| 言語 | eng |
| 内容記述 | As part of the NASA/Navy Abrupt Wing Stall Program, a relatively low-cost, rapid-access wind-tunnel free-to-roll rig was developed. This rig combines the use of conventional models and test apparatuses to evaluate both transonic performance and wing-drop/rock tendencies in a single tunnel entry. A description of the test hardware as well as a description of the experimental procedures is given. The free-to-roll test rig has been used successfully to assess the static and dynamic characteristics of three different configurations--two configurations that exhibit uncommanded lateral motions, (pre-production F/A-18E and AV-8B), and one that did not (F/A-18C). |
| NASA分類 | Acoustics |
| レポートNO | AIAA Paper 2003-0749 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/90654 |
