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Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzleBecause of the relatively high takeoff speeds of supersonic transport aircraft, it is important to know if the flight velocity affects the noise level of suppressor nozzles. To investigate this, a modified F-106B aircraft was used to conduct a series of flyover and static tests on a 48-tube suppressor installed on an uncooled plug nozzle. Comparison of flyover and static spectra indicated that flight velocity had little effect on the noise suppression of the 48-tube suppressor configuration. However, flight velocity adversely affected noise suppression of the 48-tube suppressor with an acoustic shroud and plug installed.
Document ID
19740007352
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burley, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Head, V. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
E-7513
NASA-TM-X-2919
Report Number: E-7513
Report Number: NASA-TM-X-2919
Accession Number
74N15465
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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