Aeroacoustic Improvements to Fluidic Chevron Nozzles
Author:
Affiliation:
1. NASA Langley Research Center
2. General Electric Company
3. Goodrich Aerostructures
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2706
Reference9 articles.
1. Tabs and mixers for reducing low bypass ratio jet noise
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