| タイトル | Impact of active controls technology on structural integrity |
| 著者（英） | Donley, Shawn; Austin, Edward; Noll, Thomas; Graham, George; Harris, Terry |
| 著者所属（英） | Army Avionics Research and Development Activity|NASA Langley Research Center|National Defence Headquarters|Air Force Wright Research and Development Center|Naval Air Development Center |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | This paper summarizes the findings of The Technical Cooperation Program to assess the impact of active controls technology on the structural integrity of aeronautical vehicles and to evaluate the present state-of-the-art for predicting the loads caused by a flight-control system modification and the resulting change in the fatigue life of the flight vehicle. The potential for active controls to adversely affect structural integrity is described, and load predictions obtained using two state-of-the-art analytical methods are given. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 91A32019
AIAA PAPER 91-0988 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/349009 |
