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Parallel-Plate Acoustic Absorbers For Hot EnvironmentsStacking patterns and materials chosen to suppress noise. Acoustic liners incorporating parallel-plate absorbing elements proposed for use in suppressing broadband aerodynamic noise originating in flows of hot gases in ducts. One potential application lies in suppressing noise generated in exhaust-jet mixer/ejectors in propulsion system of proposed High-Speed Civil Transport. In addition, such absorbers useful in any situation in which high temperature limits use of such conventional resonant acoustic-liner materials as perforated face sheets bonded to honey-comb-core panels.
Document ID
19950070397
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Doychak, Joseph
(NASA Lewis Research Center, Cleveland, OH.)
Parrot, Tony L.
(Langley Research Center)
Date Acquired
August 16, 2013
Publication Date
November 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 11
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15430
Accession Number
95B10576
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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