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“Notes on the Results of Recent Tests of a Momentum Exchange Type Silencer for Turbojet Engines”
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English
Abstract
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.
Authors
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.Also In
References
- “Inflight Turbojet Noise Suppression Studies” Stringas E. Auer H. June 1959
- “Fundamental Inflight Noise Suppression Research and Experimentation” Sobel J. January 1959
- “On Sound Generated Aerodynamically” Lighthill, M. J. November 13 1951