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Measurements and Predictions for a Distributed Exhaust NozzleThe acoustic and aerodynamic performance characteristics of a distributed exhaust nozzle (DEN) design concept were evaluated experimentally and analytically with the purpose of developing a design methodology for developing future DEN technology. Aerodynamic and acoustic measurements were made to evaluate the DEN performance and the CFD design tool. While the CFD approach did provide an excellent prediction of the flowfield and aerodynamic performance characteristics of the DEN and 2D reference nozzle, the measured acoustic suppression potential of this particular DEN was low. The measurements and predictions indicated that the mini-exhaust jets comprising the distributed exhaust coalesced back into a single stream jet very shortly after leaving the nozzles. Even so, the database provided here will be useful for future distributed exhaust designs with greater noise reduction and aerodynamic performance potential.
Document ID
20010047489
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kinzie, Kevin W.
(NASA Langley Research Center Hampton, VA United States)
Brown, Martha C.
(NASA Langley Research Center Hampton, VA United States)
Schein, David B.
(Northrop Grumman Corp. El Segundo, CA United States)
Solomon, W. David, Jr.
(Northrop Grumman Corp. El Segundo, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2001-2236
Report Number: AIAA Paper 2001-2236
Meeting Information
Meeting: 7th AIAA/CEAS Aeroacoustic Conference
Location: Maastricht
Country: Netherlands
Start Date: May 28, 2001
End Date: May 30, 2001
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available