Acoustics and thrust of separate-flow exhaust nozzles with mixing devices for high-bypass-ratio engines
- 12 June 2000
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Aircraft NoisePublished by Cambridge University Press (CUP) ,1989
- Aircraft Turbofan NoiseJournal of Turbomachinery, 1987