Active jet noise reduction by oscillating mechanical flaps at the nozzle exit
18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Nozzle Exit Flow Profile Shaping for Jet Noise Reduction
AIAA | 1977
|Active Control of Turbomachine Discrete Frequency Noise Utilizing Oscillating Flaps and Pistons
British Library Conference Proceedings | 1995
|Active Control of Turbomachine Discrete Frequency Noise Utilizing Oscillating Flaps and Pistons
Online Contents | 1997
|Nozzle exit flow profile shaping for jet noise reduction
AIAA | 1976
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