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NASA NTRS · 19900059922

Active control of structurally-coupled sound fields in elastic cylinders by vibrational force inputs

Abstract

Active control of structurally-coupled sound fields in elastic cylinders is analytically and experimentally studied. The primary (noise) field in the cylinder model is generated by the coupled dynamic response of the shell under loading by a single exterior acoustic source. Control of the interior sound field is achieved by applying vibrational force inputs directly to the shell wall. Action of the point controllers serve to increase the input impedance of select structural modes of the shell which are well-coupled to the interior acoustic cavity, thus substantially reducing sound transmission into the cavity. Spatially-averaged noise reductions in excess of 30 dB are demonstrated for acoustic resonant conditions within the cavity. Twin controller configurations are presented which demonstrate the ability to independently control orthogonal modes of the interior acoustic space. Benefits and drawbacks of this new methodology for noise control are discussed and clearly demonstrated.

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BibTeXRIS

Jones, J. D., Fuller, C. R.. 1990-07-01. Active control of structurally-coupled sound fields in elastic cylinders by vibrational force inputs. https://ntrs.nasa.gov/citations/19900059922

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