“Notes on the Results of Recent Tests of a Momentum Exchange Type Silencer for Turbojet Engines” 600301
Presented in this paper is a brief review of momentum exchange theory for Jet Noise Suppression. “Experimental Results from Scale Model Tests” are included. These data exhibit peak to peak attenuation of 20 db along maximum exhaust noise azimuths at a nozzle pressure ratio of 3.1.
Citation: STRINGAS, E., "“Notes on the Results of Recent Tests of a Momentum Exchange Type Silencer for Turbojet Engines”," SAE Technical Paper 600301, 1960, https://doi.org/10.4271/600301. Download Citation
Author(s):
E. STRINGAS
Pages: 16
Event:
Pre-1964 SAE Technical Papers
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Turbojet engines
Scale models
Noise
Technical review
Nozzles
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