7th AIAA/CEAS Aeroacoustics Conference and Exhibit 2001
DOI: 10.2514/6.2001-2230
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Interior noise reduction of composite cylinders using distributed vibration absorbers

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Cited by 10 publications
(7 citation statements)
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“…These include source reduction methods, active [4,5] and passive [6,7] control of the aircraft transmission paths as well as the active control of the sound field [8,9]. Another approach is to install (partially damped) resonant devices such as Helmholtz resonators and distributive vibration absorbers [10][11][12] to reduce the fuselage vibrations or to damp the cabin's acoustic resonances.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…These include source reduction methods, active [4,5] and passive [6,7] control of the aircraft transmission paths as well as the active control of the sound field [8,9]. Another approach is to install (partially damped) resonant devices such as Helmholtz resonators and distributive vibration absorbers [10][11][12] to reduce the fuselage vibrations or to damp the cabin's acoustic resonances.…”
Section: Introductionmentioning
confidence: 99%
“…They have been proven to offer broad-band control of noise transmission into cylinders [10,12] due to the fact that they combine two effects: acoustic absorption by the acoustic foam (elastic layer) at high frequencies and the reduction of efficiently sound radiating structural modes at low frequencies. HG blankets represent an extension of this idea by distributing the dynamic vibration absorbers over the whole structure by inserting a number of masses into the elastic material which blankets the entire structure (or large portions of the structure).…”
Section: Introductionmentioning
confidence: 99%
“…Using a variety of mass area densities and by altering the effective spring transverse stiffness by changing the woven layer characteristics, DVAs can be tuned over a large range of frequencies. The DVA was recently studied by Marcotte 2 in depth and has been applied to a variety of structures, for instance large cylindrical shells 3,4 .…”
Section: Introductionmentioning
confidence: 99%
“…Due to the difficulties of predicting acoustic resonance using analytical or numerical methods, much of the work has been conducted experimentally, similar to the shaker excitations used for modal extraction in structural engineering. A classical approach to establish possible links between observed instabilities and acoustic resonances is based on white-noise excitation of the component under study and the filtering of acoustic resonance frequencies by using loudspeakers [10][11][12][13][14]. In many cases, such experimental simple acoustic characterization may well provide crucial information about flow-induced resonant sound generation during operating conditions [15,16].…”
Section: Introductionmentioning
confidence: 99%