NASA NTRS · 19910055203
Short conical solid/perforated plug-nozzle as supersonic jet noise suppressor
Abstract
Experimental studies of the acoustic far field, and the nature of the repetitive shock structure in cold jet flows from an externally expanded plug-nozzle having a short conical plug with a pointed termination, operated in a range of supercritical pressure ratios of 2.0 to 4.5, are reported. The overall sound pressure levels of a short solid conical plug-nozzle (CPN) are found to be within 3 dB of those of the baseline noise levels of a minimum length contoured plug-nozzle operated at the same pressure ratio and having the same annular throat area. As compared to an equivalent convergent nozzle, the noise reductions achieved through the use of a short solid CPN are of the order of 5 dB.
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Das, I. S., Dosanjh, D. S.. 1991-05-08. Short conical solid/perforated plug-nozzle as supersonic jet noise suppressor. https://ntrs.nasa.gov/citations/19910055203
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