NASA NTRS · 19850000368
Low-Noise Supersonic Nozzle
Abstract
Two-dimensional nozzle incorporates unusual design features of rapid expansion contour, boundary-layer bleed slots upstream of throat, and exit width-to-height ratio of 1.7 to provide noise levels in upstream regions of test rhombus substantially lower than in conventional nozzles.
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Beckwith, I. E.. 1986-01-01. Low-Noise Supersonic Nozzle. https://ntrs.nasa.gov/citations/19850000368
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