| タイトル | Ground vibration test results for Drones for Aerodynamic and Structural Testing (DAST)/Aeroelastic Research Wing (ARW-1R) aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860009841 |
| 著者（英） | Gilyard, G. B.; Cox, T. H. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | The drones for aerodynamic and structural testing (DAST) project was designed to control flutter actively at high subsonic speeds. Accurate knowledge of the structural model was critical for the successful design of the control system. A ground vibration test was conducted on the DAST vehicle to determine the structural model characteristics. This report presents and discusses the vibration and test equipment, the test setup and procedures, and the antisymmetric and symmetric mode shape results. The modal characteristics were subsequently used to update the structural model employed in the control law design process. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 86N19312
NAS 1.15:85906
NASA-TM-85906
H-1261 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/154767 |
