NASA NTRS · 19940028983
New broadband shock noise model and computer code for ANOPP
Abstract
The basic mechanism for broadband shock noise in supersonic jets is the interaction between the shock waves and the turbulence in the jet exhaust. This source is in addition to jet mixing noise.
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Reddy, N. N.. 1992-04-01. New broadband shock noise model and computer code for ANOPP. https://ntrs.nasa.gov/citations/19940028983
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