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High Temperature Acoustic Liner TechnologyThis paper describes work currently in progress at Langley on liner concepts that employ structures that may be suitable for broadband exhaust noise attenuation in high speed flow environments and at elevated temperatures characteristic of HSCT applications. Because such liners will need to provide about 10 dB suppression over a 2 to 3 octave frequency range, conventional single-degree-of-freedom resonant structures will not suffice. Bulk absorbers have the needed broadband absorption characteristic; however, at lower frequencies they tend to be inefficient.
Document ID
19990110639
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Parrott, Tony L.
(NASA Langley Research Center Hampton, VA United States)
Jones, Michael G.
(Lockheed Engineering and Sciences Co. Hampton, VA United States)
Posey, Joe W.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
September 1, 1999
Publication Information
Publication: First NASA/Industry High Speed Research Program Nozzle Symposium
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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