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Hybrid Damping System for an Electronic Equipment Mounting ShelfThe objective of this study was to design and construct a vibration control system for an electronic equipment shelf to be evaluated in the NASA Dryden FTF-11. The vibration control system was a hybrid system which included passive and active damping techniques. Passive damping was fabricated into the equipment shelf using ScothDamp(trademark) damping film and aluminum constraining layers. Active damping was achieved using a two channel active control circuit employing QuickPack(trademark) sensors and actuators. Preliminary Chirp test results indicated passive damping smoothed the frequency response while active damping reduced amplitudes of the frequency response for most frequencies below 500Hz.
Document ID
19970026247
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Voracek, David
(NASA Dryden Flight Research Center Edwards, CA United States)
Kolkailah, Faysal A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Cavalli, J. R.
(NASA Dryden Flight Research Center Edwards, CA United States)
Elghandour, Eltahry
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Engineering (General)
Report/Patent Number
NASA-CR-204539
NAS 1.26:204539
Accession Number
97N25578
Funding Number(s)
CONTRACT_GRANT: NCC2-5110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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