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NASA NTRS · 19910045799

Active control of sound radiation from a vibrating rectangular panel by sound sources and vibration inputs - An experimental comparison

Abstract

Active control of sound radiation from a rectangular panel by two different methods has been experimentally studied and compared. In the first method a single control force applied directly to the structure is used with a single error microphone located in the radiated acoustic field. Global attenuation of radiated sound was observed to occur by two main mechanisms. For 'on-resonance' excitation, the control force had the effect of increasing the total panel input impedance presented to the nosie source, thus reducing all radiated sound. For 'off-resonance' excitation, the control force tends not significantly to modify the panel total response amplitude but rather to restructure the relative phases of the modes leading to a more complex vibration pattern and a decrease in radiation efficiency. For acoustic control, the second method, the number of acoustic sources required for global reduction was seen to increase with panel modal order. The mechanism in this case was that the acoustic sources tended to create an inverse pressure distribution at the panel surface and thus 'unload' the panel by reducing the panel radiation impedance. In general, control by structural inputs appears more effective than control by acoustic sources for structurally radiated noise.

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BibTeXRIS

Fuller, C. R., Hansen, C. H., Snyder, S. D.. 1991-03-08. Active control of sound radiation from a vibrating rectangular panel by sound sources and vibration inputs - An experimental comparison. https://ntrs.nasa.gov/citations/19910045799

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