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Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzleAt the relatively high takeoff speeds of supersonic transport aircraft, an important question concerns whether the flight speed affects the noise of suppressor nozzles. To answer this question, flyover and static tests using a modified F-106B aircraft were conducted on a 104-tube suppressor nozzle. Comparison of adjusted flyover and static spectra indicated that flight velocity had a small adverse effect on the suppression of the 104-tube suppressor. The adverse effect was larger with the acoustic shroud installed than without it.
Document ID
19740020127
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burley, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-3049
E-7901
Report Number: NASA-TM-X-3049
Report Number: E-7901
Accession Number
74N28240
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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