Abstract
Acoustic attenuation of lightweight structures is one way of lowering payload cost of launch vehicles. This paper describes results of a study to determine the effectiveness of high structural damping to reduce low frequency noise. Both passive and active damping techniques were examined. Passive damping was achieved using a surface bonded constrained layer damping treatment and active damping was achieved with surface bonded piezoceramic wafers and a closed-loop controller. The paper discusses the analytical models used to predict noise reduction of a large flat panel and show comparisons with test data. Finite element models using NASTRAN and vibro-acoustic models using SYSNOISE were used to predict noise reduction. A test bed made of a large flat composite panel mounted as one wall of a very stiff six-sided enclosure was constructed. The enclosure and panel was placed in an acoustic chamber and subjected to a high acoustic environment.
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