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Resonant Interaction of a Linear Array of Supersonic Rectangular Jets: an Experimental StudyThis paper examines a supersonic multi jet interaction problem that we believe is likely to be important for mixing enhancement and noise reduction in supersonic mixer-ejector nozzles. We demonstrate that it is possible to synchronize the screech instability of four rectangular jets by precisely adjusting the inter jet spacing. Our experimental data agrees with a theory that assumes that the phase-locking of adjacent jets occurs through a coupling at the jet lip. Although the synchronization does not change the frequency of the screech tone, its amplitude is augmented by 10 dB. The synchronized multi jets exhibit higher spreading than the unsynchronized jets, with the single jet spreading the least. We compare the nearfield noise of the four jets with synchronized screech to the noise of the sum of four jets operated individually. Our noise measurements reveal that the more rapid mixing of the synchronized multi jets causes the peak jet noise source to move up stream and to radiate noise at larger angles to the flow direction. Based on our results, we believe that screech synchronization is advantageous for noise reduction internal to a mixer-ejector nozzle, since the noise can now be suppressed by a shorter acoustically lined ejector.
Document ID
19950009437
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Raman, Ganesh
(NYMA, Inc. Brook Park, OH, United States)
Taghavi, Ray
(NYMA, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-195398
NAS 1.26:195398
E-9128
Report Number: NASA-CR-195398
Report Number: NAS 1.26:195398
Report Number: E-9128
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Start Date: January 9, 1994
End Date: January 12, 1994
Accession Number
95N15852
Funding Number(s)
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 537-02-22
Distribution Limits
Public
Copyright
Public Use Permitted.
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