Experimental study for multi-lobed mixer high bypass exhaust systems for subsonic jet noise reduction. II - Acoustic results
5th AIAA/CEAS Aeroacoustics Conference and Exhibit ; 1999 ; Bellevue , WA , U.S.A.
01.01.1999
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Measurements of the Subsonic Lobed Mixer Flowfield
British Library Conference Proceedings | 1997
|LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
Europäisches Patentamt | 2022
|LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
Europäisches Patentamt | 2022
|LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
Europäisches Patentamt | 2022
|