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Aeroacoustics of contoured and solid/porous conical plug-nozzle supersonic jet flowsThe acoustic far field, the shock-associated noise and characteristics of the repetitive shock structure of supersonic jet flows issuing from a contoured plug-nozzle and uncontoured plug-nozzle having a short conical plug of either a solid or a combination of solid/porous surface with pointed termination operated at a range of supercritical pressure are reported. The contoured and the uncontoured plug-nozzles had the same throat area and the same annular-radius ratio.
Document ID
19860012837
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dosanjh, D. S.
(Syracuse Univ. NY, United States)
Das, I. S.
(Syracuse Univ. NY, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1985
Subject Category
Acoustics
Report/Patent Number
NASA-CR-176645
NAS 1.26:176645
Report Number: NASA-CR-176645
Report Number: NAS 1.26:176645
Accession Number
86N22308
Funding Number(s)
CONTRACT_GRANT: NAG1-29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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