| タイトル | The impact of active controls technology on the structural integrity of aeronautical vehicles |
| 著者（英） | Graham, George; Donley, Shawn; Lee, Ben; Kaynes, Ian; Harris, Terry; Sparrow, James; Noll, Thomas E.; Austin, Edward |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-04-01 |
| 言語 | eng |
| 内容記述 | The findings of an investigation conducted under the auspices of The Technical Cooperation Program (TTCP) 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 loads caused by a flight-control system modification and the resulting change in the fatigue life of the flight vehicle are summarized. Important points concerning structural technology considerations implicit in applying active controls technology in new aircraft are summarized. These points are well founded and based upon information received from within the aerospace industry and government laboratories, acquired by sponsoring workshops which brought together experts from contributing and interacting technical disciplines, and obtained by conducting a case study to independently assess the state of the technology. The paper concludes that communication between technical disciplines is absolutely essential in the design of future high performance aircraft. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 94N11341 |
| 権利 | Copyright, Distribution within the U.S. granted by agreement |
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