NASA NTRS · 20160007307
Acoustic Panel Liner for an Engine Nacelle
Abstract
An acoustic panel liner includes a face sheet, back plate, and liner core positioned there-between, which may be used in an engine nacelle. Elongated chambers contain variable amounts of septa at a calibrated depth or depths. The septa may have varying DC flow resistance. The chambers may have a hexagonal or other polygonal cross sections. The septa, such as mesh caps, may be bonded to an inner wall of a corresponding chamber. The insertion depths may be the same or different. If different, the pattern of distribution of the depths may be randomized.
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Jones, Michael G., Nark, Douglas M., Ayle, Earl, Ichihashi, Fumitaka. 2016-05-10. Acoustic Panel Liner for an Engine Nacelle. https://ntrs.nasa.gov/citations/20160007307
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