| タイトル | Evaluating Attenuation of Vibration Response using Particle Impact Damping for a Range of Equipment Assemblies |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130013857 |
| 著者（英） | Smith, Andrew; Knight, Brent; Hunt, Ron; Craigmyle, Ben; Towner, Robert; LaVerde, Bruce; Parsons, David |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2013-04-08 |
| 言語 | eng |
| 内容記述 | Particle dampers provide a mechanism for diverting energy away from resonant structural vibrations. This experimental study provides data from a series of acoustically excited tests to determine the effectiveness of these dampers for equipment mounted to a curved orthogrid panel for a launch vehicle application. Vibration attenuation trends are examined for variations in particle damper fill level, component mass, and excitation energy. A significant response reduction at the component level was achieved, suggesting that comparatively small, strategically placed, particle damper devices might be advantageously used in launch vehicle design. These test results were compared to baseline acoustic response tests without particle damping devices, over a range of isolation and damping parameters. Instrumentation consisting of accelerometers, microphones, and still photography data will be collected to correlate with the analytical results. |
| NASA分類 | Acoustics |
| レポートNO | M12-2109 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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