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Apparatus and method for jet noise suppressionA method and apparatus for jet noise suppression through control of the static pressure of the jet and control of the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle is disclosed. The momentum flux over an extended region of the jet is regulated, affecting Reynolds stresses in the jet and the spreading angle of the jet. Static pressure is controlled through a long hollow, porous nozzle plug centerbody which may be selectively vented to ambient conditions, connected to a vacuum source, or supplied with fluids of various densities for injection into the stream. Sound in the jet may be channeled along the nozzle plug centerbody by injecting coolant such as a cryogenic fluid throughout the center-body into the jet.
Document ID
19840006805
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Maestrello, L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 16, 1983
Subject Category
Acoustics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-238791
Patent Number: US-PATENT-4,398,667
Patent Number: NASA-CASE-LAR-11903-2
Patent Application Number: US-PATENT-APPL-SN-753971
Accession Number
84N14873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,398,667|NASA-CASE-LAR-11903-2
Patent Application
US-PATENT-APPL-SN-238791|US-PATENT-APPL-SN-753971
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