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Evaluating Attenuation of Vibration Response using Particle Impact Damping for a Range of Equipment AssembliesParticle 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.
Document ID
20130013857
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Knight, Brent
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Parsons, David
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Smith, Andrew
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hunt, Ron
(Bevilacqua Research Corp. Huntsville, AL, United States)
LaVerde, Bruce
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Towner, Robert
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Craigmyle, Ben
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
April 8, 2013
Subject Category
Acoustics
Report/Patent Number
M12-2109
Report Number: M12-2109
Meeting Information
Meeting: AIAA Aerospace Design and Structures Event
Location: Boston, MA
Country: United States
Start Date: April 8, 2013
End Date: April 11, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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