"Notes on the Results of Recent Tests of a Momentum Exchange Type Silencer for Turbojet Engines"

Format:

Conference/Event

Author/Creator:

STRINGAS, E., author.

Conference Name:

For presentation at the SAE NATIONAL AERONAUTIC MEETING

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1960

Summary:

SynopsisPresented 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.

Notes:

Vendor supplied data

Publisher Number:

600301

Access Restriction:

Restricted for use by site license