Variable Geometry Chevrons for Jet Noise Reduction
- 8 May 2006
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community NoisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Effect of Uniform Chevrons on Cruise Shockcell NoisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Fiber-Optic Shape Sensing and Distributed Strain Measurements on a Morphing ChevronPublished 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
- Acoustic Investigation of a High Bypass Ratio Separate Flow Exhaust System with ChevronsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2004
- Subsonic Jet Noise Reduction Variable Geometry ChevronPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2004
- Evaluating the Impact of Morphing Technologies on Aircraft PerformancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2002
- Jet Noise: Since 1952Theoretical and Computational Fluid Dynamics, 1998