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Trapped Waves and Screech Tones With Various Rectangular NozzlesThis report documents experimental observations made on ‘trapped waves’ occurring with various convergent, rectangular nozzles. Most of the data pertain to three nozzles of aspect ratios (AR) 2, 4 and 8, each having an equivalent diameter of 2.12 in. The trapped waves, manifesting as a series of peaks in the near field pressure fluctuation spectra, are seen with all three nozzles. The number of spectral peaks detected on the major axis is larger than that detected on the minor axis by a factor approximately equal to the AR. These spectral peaks occur in high subsonic conditions and persist into the supersonic regime. Screech tones seem to appear as a continuation of these spectral peaks, i.e., with increasing Mach number it is as if one of these peaks gets amplified and turns into the screech tone. This trend is clearer at smaller AR and gets somewhat obscured at higher AR. Screech frequency variation with Mach number is documented for these and other rectangular nozzles, covering an AR range of 1-16. For larger AR (≥ 3), screech frequency is found to scale on the narrow dimension of the nozzle. Screech staging behavior is more pronounced for smaller AR cases. The screech frequency data for the AR=1 (square) case involves multiple stages similar to that of a round nozzle.
Document ID
20210015372
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
K B M Q Zaman
(Glenn Research Center Cleveland, Ohio, United States)
A F Fagan
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 11, 2021
Publication Date
May 21, 2021
Subject Category
Aeronautics (General)
Report/Patent Number
E-19946
NASA/TM-20210015372
Funding Number(s)
WBS: 109492.02.03.09.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
nozzles
jet instability
noise
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