| タイトル | Preliminary results of experimental and analytical investigations of the tumbling phenomenon for an advanced configuration |
| 著者（英） | Croom, M. A.; Fears, S. P.; Whipple, R. D. |
| 著者所属（英） | Joint Inst. for Advancement of Flight Sciences|NASA Langley Research Center |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | A sustained autorotative pitching motion usually called 'tumbling' has been observed during dynamic model tests of the X-29A configuration. The X-29 is an advanced design incorporating forward-swept wings and canards in a highly relaxed static stability condition. Beginning with a historical review of the tumbling phenomenon, this paper discusses the current experimental results of dynamic model tumbling tests of the X-29 and the initial efforts to establish an aerodynamic and mathematical model for analysis. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 84A42376
AIAA PAPER 84-2108 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/397031 |
