An experimental model investigation of turbofan engine internal exhaust gas mixer configurations
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Nozzle exit flow profile shaping for jet noise reductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Jet noise characteristics of unsuppressed duct burning turbofan exhaust systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Practical Bypass Mixing Systems for Fan Jet Aero EnginesAeronautical Quarterly, 1966