Effect of Uniform Chevrons on Cruise Shockcell Noise
- 8 May 2006
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Variable Geometry Chevrons for Jet Noise ReductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Acoustic and Flow-Field Characteristics of Shock-cell Noise from Dual Flow NozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Stochastic model theory of broadband shock associated noise from supersonic jetsJournal of Sound and Vibration, 1987
- Shock associated noise of supersonic jets from convergent-divergent nozzlesJournal of Sound and Vibration, 1982