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NASA NTRS ยท 19800043284

Sound propagation through parallel jets exhausting from ducts

Abstract

The method of matched asymptotic expansions is employed to construct the solution for the propagation of sound through parallel jets which exit from long ducts and are surrounded by a uniform parallel stream. Parts of the duct walls are lined with acoustically absorbent material. The small parameter for the expansion is the ratio of the inner jet thickness to the accoustic wavelength. The problem is further simplified when the condition is imposed that the speed of the outer stream, which accounts for the forward motion speed of the ducts, is much smaller than the speeds of the jets. This condition is valid during landing and takeoff operations. Farfield pressure distributions are obtained for the case in which the inner jet is much faster than the outer jet and the case in which the two jets are the same.

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BibTeXRIS

Ting, L.. 1980-03-01. Sound propagation through parallel jets exhausting from ducts. https://ntrs.nasa.gov/citations/19800043284

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