We report the results of tests conducted to demonstrate the effectiveness of active vibration control techniques in reducing structure borne noise in aircraft cabins. A prototype active vibration control system was tested in the Douglas Aircraft Company Fuselage Acoustic Research Facility, using the aft section of a DC-9 aircraft as the test article
No takes yet. Share an insight, caveat, or question.
Simpson et al. (1991) studied this question.
Synapse has enriched one closely related paper. Consider it for comparative context: