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Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppressionA three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle designed to reduce the jet noise created at takeoff by a future supersonic transport. The PARC3D computational fluid dynamics (CFD) code was used to study the flow field of the nozzle. The grid that was used in the analysis consisted of approximately 900,000 node points contained in eight grid blocks. Two nozzle configurations were studied: a constant area mixing section and a diverging mixing section. Data are presented for predictions of pressure, velocity, and total temperature distributions and for evaluations of internal performance and mixing effectiveness. The analysis provided good insight into the behavior of the flow.
Document ID
19920071435
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Debonis, James R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 92-3570
Accession Number
92A54059
Distribution Limits
Public
Copyright
Other

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